Encyclopedia Astronautica
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KAUR-4
Modern satellite bus for Russian geosynchronous satellites. Developed in the 1980's, and only reached flight status in the 1990's after the fall of the Soviet Union. The bus provided the basis for the Gals, Ekspress, and Yamal communications and direct broadcast satellites.
Subtopics
 | Potok Russian military communications satellite. Potok was one element of the second generation global command and control system (GKKRS) developed according to a decree of 17 February 1976. |
 | Luch Russian military communications satellite. |
| Forpost Russian military communications satellite. Study 1992. Communications satellite - Soviet Ministry of Defense. No other details available. |
 | Gals Russian communications satellite. Direct broadcasting satellite (new generation of satellites) intended for development of the Russian television system and international cooperation. |
 | Ekspress Russian communications satellite. The Ekspress series communications satellite closely resembled the Gals spacecraft and shared a similar spacecraft bus. |
 | Yamal Russian communications satellite. The Yamal communications satellite bus was developed by RKK Energia for Gazprom. |
1982 May 17 - .
23:50 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM.
1984 March 2 - .
03:54 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/40.
LV Family: Proton.
Launch Vehicle: Proton-K/DM.
1985 October 25 - .
15:45 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/40.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
1986 April 4 - .
03:45 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/40.
LV Family: Proton.
Launch Vehicle: Proton-K/DM.
1987 October 1 - .
17:09 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
1987 November 26 - .
13:28 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
- Cosmos 1897 - .
Payload: Luch s/n 12L. Mass: 2,000 kg (4,400 lb). Nation: Russia.
Agency: MOM.
Class: Communications.
Type: Military communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Luch .
Completed Operations Date: 1992-10-01 . USAF Sat Cat: 18575 . COSPAR: 1987-096A. Apogee: 35,790 km (22,230 mi). Perigee: 35,763 km (22,222 mi). Inclination: 3.8000 deg. Period: 1,435.60 min.
Stationed at 95 deg E. Relaying of telephone and telegraph information. Second launch in Altair/SR system for communication with Mir space station and other orbital spacecraft. In late July 1988 Cosmos 1897 was moved from its station at 95 degrees East to 12 degrees East to support the Buran shuttle test flight of November 14, 1988. During February 1987 the satellite was moved back to its original position at 95 degrees East. The satellite drifted to 90 degrees East by March 1991. By late April it was maneuvered it back to 95 degrees East, but by the end of 1991 it had drifted to 77 degrees East and was considered inoperative. Positioned in geosynchronous orbit at 95 deg E in 1987-1988; 12 deg E in 1988-1989; 95 deg E in 1989-1992 As of 5 September 2001 located at 62.12 deg E drifting at 0.168 deg W per day. As of 2007 Mar 10 located at 94.48E drifting at 0.087E degrees per day.
1988 August 1 - .
21:04 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
- Cosmos 1961 - .
Payload: Potok no. 5 s/n 16L. Mass: 2,000 kg (4,400 lb). Nation: Russia.
Agency: MOM.
Class: Communications.
Type: Military communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Potok.
Completed Operations Date: 1993-12-15 . USAF Sat Cat: 19344 . COSPAR: 1988-066A. Apogee: 35,796 km (22,242 mi). Perigee: 35,780 km (22,230 mi). Inclination: 8.6000 deg. Period: 1,436.20 min.
Stationed at 13.5 deg W; later moved to 80 deg E. Investigation of outer space and relay of telegraph and telephone messages. Positioned in geosynchronous orbit at 14 deg W in 1988-1992; 80 deg E in 1992-1993. In September, 1993, Cosmos 1961 began drifting off station after a mission of five years had apparently been terminated. As of 4 September 2001 located at 80.01 deg E drifting at 0.015 deg W per day. As of 2007 Mar 11 located at 74.58E drifting at 0.039E degrees per day.
1989 December 27 - .
11:10 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
- Cosmos 2054 - .
Payload: Luch s/n 14L. Mass: 2,150 kg (4,730 lb). Nation: Russia.
Agency: MOM.
Class: Communications.
Type: Military communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Luch .
Completed Operations Date: 1997-03-01 . USAF Sat Cat: 20391 . COSPAR: 1989-101A. Apogee: 35,822 km (22,258 mi). Perigee: 35,777 km (22,230 mi). Inclination: 7.7000 deg. Period: 1,436.80 min.
Stationed at 346 deg E. Relaying of telegraph and telephone information. The third Altair/SR geosynchronous satellite for communication with Mir space station and other orbital spacecraft. Combined with Cosmos 1897, it permitted Mir to maintain contact with Mission Control in Moscow 70% of the time. Positioned in geosynchronous orbit at 16 deg W in 1990-1997 As of 30 August 2001 located at 21.03 deg W drifting at 0.023 deg E per day. As of 2007 Mar 9 located at 68.57W drifting at 0.338W degrees per day.
1990 July 18 - .
21:46 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
1991 November 22 - .
13:27 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC81/23.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
1994 January 20 - .
09:49 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC81/23.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2M.
1994 September 21 - .
17:53 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
- Cosmos 2291 - .
Payload: Potok no. 8 s/n 19L. Mass: 2,300 kg (5,000 lb). Nation: Russia.
Agency: MOM.
Class: Communications.
Type: Military communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Potok.
USAF Sat Cat: 23267 . COSPAR: 1994-060A. Apogee: 35,829 km (22,263 mi). Perigee: 35,774 km (22,228 mi). Inclination: 4.5000 deg. Period: 1,436.90 min.
Cosmos 2291 quickly moved to 80 degrees E, joining Cosmos 2085 as a replacement for Cosmos1961. Thus, at the end of 1994 the Potok constellation had been restored to its normal 4�sateellite complement: Cosmos 2085 and 2291 at 80 degrees E and Cosmos 1888 and 2172 at 13.5 degrees W. Cosmos 2291 continued at 80 deg E in 1994-1995; then it was moved to 14 deg W in 1995-1999 As of 6 September 2001 located at 62.64 deg W drifting at 0.324 deg W per day. As of 2007 Mar 10 located at 112.35W drifting at 0.417W degrees per day.
1994 October 13 - .
16:19 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2M.
1994 December 16 - .
12:00 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC81/23.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
1995 August 30 - .
19:33 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
1995 October 11 - .
16:26 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC81/23.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
1995 November 17 - .
14:25 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
1996 September 26 - .
17:50 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2M.
- Ekspress No. 12 - .
Payload: Ekspress s/n 12L. Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: AO Infor.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Gals.
USAF Sat Cat: 24435 . COSPAR: 1996-058A. Apogee: 35,809 km (22,250 mi). Perigee: 35,779 km (22,231 mi). Inclination: 3.5000 deg. Period: 1,436.50 min. Stationed at 80.0 deg E. Positioned in geosynchronous orbit at 80 deg E in 1996-1999 As of 5 September 2001 located at 103.84 deg E drifting at 0.012 deg W per day. As of 2007 Mar 10 located at 82.98E drifting at 0.225W degrees per day..
1999 September 6 - .
16:36 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC81/23.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2M.
- Yamal 101 - .
Mass: 1,360 kg (2,990 lb). Nation: Russia.
Agency: AO Gazco.
Manufacturer: Korolev bureau.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Yamal.
USAF Sat Cat: 25896 . COSPAR: 1999-047A. Apogee: 36,298 km (22,554 mi). Perigee: 35,503 km (22,060 mi). Inclination: 2.4000 deg. Period: 1,441.90 min.
The first two Yamal communications satellites were placed into a 197 km x 36,311 km x 49.3 degree transfer orbit The DM-2M fourth stage made two successful burns, placing the satellites in circular 36,000 km geosynchronous orbits. Yamal 101 reportedly ran into problems after it was deployed. RKK Energia built the new Yamal satellites for AO Gazcom of Moscow, a joint venture of RKKE and RAO Gazprom, the Russian natural gas monopoly. The two satellites will support internal communications for RAO Gazprom. Positioned in geosynchronous orbit at 89 deg E in 1999. As of 30 August 2001 located at 112.86 deg E drifting at 1.484 deg W per day. As of 2007 Mar 10 located at 42.96E drifting at 1.484W degrees per day.
- Yamal 102 - .
Mass: 1,360 kg (2,990 lb). Nation: Russia.
Agency: AO Gazco.
Manufacturer: Korolev bureau.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Yamal.
Completed Operations Date: 1999-09-01 . USAF Sat Cat: 25897 . COSPAR: 1999-047B. Apogee: 35,802 km (22,246 mi). Perigee: 35,772 km (22,227 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Geosynchronous communications satellite. Stationed at 90 deg E. As of 5 September 2001 located at 89.85 deg E drifting at 0.005 deg W per day. As of 2007 Mar 10 located at 89.78E drifting at 0.010W degrees per day..
1999 October 27 - .
16:16 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
FAILURE: Failed early in second-stage burn.. Failed Stage: 2. - Ekspress-A1 - .
Mass: 2,500 kg (5,500 lb). Nation: Russia.
Agency: Svyaz.
Manufacturer: Reshetnev bureau.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Gals.
Communications satellite; failed to reach orbit..
2000 March 12 - .
04:07 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2M.
- Ekspress 6A - .
Payload: Ekspress A No. 2. Mass: 2,600 kg (5,700 lb). Nation: Russia.
Agency: Intersputnik.
Manufacturer: Reshetnev bureau.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Gals.
USAF Sat Cat: 26098 . COSPAR: 2000-013A. Apogee: 35,838 km (22,268 mi). Perigee: 35,736 km (22,205 mi). Inclination: 5.3000 deg. Period: 1,436.10 min.
GO Kosmicheskaya Svyaz geosynchronous communications satellite, to be assigned to the Ekspress 6A slot at 80E. Replaced the first Ekspress A, lost in a launch failure in 1999. Russian satellite bus with a ommunications payload from Alcatel France. Stationed at 80 deg E. Positioned in geosynchronous orbit at 80 deg E in 2000. As of 5 September 2001 located at 80.02 deg E drifting at 0.008 deg W per day. As of 2007 Mar 10 located at 102.77E drifting at 0.018W degrees per day.
2000 April 17 - .
21:06 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2M.
- Sesat - .
Mass: 2,500 kg (5,500 lb). Nation: Europe.
Agency: Eutelsat.
Manufacturer: Reshetnev bureau.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Ekspress.
USAF Sat Cat: 26243 . COSPAR: 2000-019A. Apogee: 35,802 km (22,246 mi). Perigee: 35,771 km (22,227 mi). Inclination: 0.1000 deg. Period: 1,436.10 min.
Sesat (Siberia-Europe Satellite) used an MSS-2500-GSO (Gals/Ekspress) satellite bus built by NPO PM of Krasnoyarsk, with an Alcatel Espace France payload of 18 Ku-band transponders. The satellite had 8 Fakel SPD-100 plasma thrusters for stationkeeping. Eutelsat operated their Hot Bird fleet of European television broadcast satellites since the 1980's, but the venture into broadcasting to Siberia represented a new step for them. Stationed at 36 deg E. Positioned in geosynchronous orbit at 39 deg E in 2000. As of 4 September 2001 located at 35.97 deg E drifting at 0.005 deg E per day. As of 2007 Mar 9 located at 35.92E drifting at 0.004E degrees per day.
2000 June 24 - .
00:28 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2M.
2000 July 4 - .
23:44 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
2002 June 10 - .
01:14 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2M.
- Ekspress A1R - .
Payload: Ekspress A No. 4. Mass: 2,600 kg (5,700 lb). Nation: Russia.
Agency: Svyaz.
Manufacturer: Reshetnev bureau.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Gals.
USAF Sat Cat: 27441 . COSPAR: 2002-029A. Apogee: 35,792 km (22,240 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.2000 deg. Period: 1,436.00 min.
Launch delayed from May 2002. The Ekspress A1R Russian domestic communications satellite was built by NPO PM and Alcatel for Kosmicheskiya Svyaz, the Russian satcom operator. The Proton's parking orbit was off-nominal but the 11S861-01 Blok DM-2M upper stage corrected for this and delivered the payload to the correct orbit. Parking orbit was about 180 x 185 km x 51.6 deg; transfer orbit after the first DM-2M burn was 328 x 36133 km x 47.4 deg; orbit at spacecraft separation was 36102 x 36171 km x 0.2 deg. Two SOZ ullage motors were left in the transfer orbit. As of 2007 Mar 10 located at 14.07W drifting at 0.008W degrees per day.
2003 November 24 - .
06:22 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC81/23.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2M.
- Yamal-200 KA-1 - .
Mass: 1,360 kg (2,990 lb). Nation: Russia.
Agency: Gazprom.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Yamal.
USAF Sat Cat: 28094 . COSPAR: 2003-053B. Apogee: 35,799 km (22,244 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Two geosynchronous communications satellites launched for Gazprom. As of 2007 Mar 11 located at 49.00E drifting at 0.012E degrees per day..
- Yamal-200 KA-2 - .
Mass: 1,320 kg (2,910 lb). Nation: Russia.
Agency: Gazprom.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Yamal.
Decay Date: 2004-09-20 . USAF Sat Cat: 28089 . COSPAR: 2003-053A. Apogee: 35,797 km (22,243 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.0300 deg. Period: 1,436.13 min. As of 2007 Mar 11 located at 90.00E drifting at 0.016W degrees per day..
2003 December 28 - .
23:00 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2M.
- Ekspress AM-22 - .
Mass: 2,542 kg (5,604 lb). Nation: Russia.
Agency: Chelomei Design Bureau.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Gals.
USAF Sat Cat: 28134 . COSPAR: 2003-060A. Apogee: 35,796 km (22,242 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.0400 deg. Period: 1,436.11 min. The Ekspress AM-22 communications satellite was built by NPO PM and Alcatel Space for GPKS, the Russian Space Communications Company. As of 2007 Mar 10 located at 52.99E drifting at 0.005W degrees per day..
2004 April 26 - .
20:37 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2M.
- Ekspress AM-11 - .
Mass: 2,542 kg (5,604 lb). Nation: Russia.
Agency: Svyaz.
Manufacturer: Cannes,
Reshetnev Design Bureau.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Gals.
USAF Sat Cat: 28234 . COSPAR: 2004-015A. Apogee: 35,788 km (22,237 mi). Perigee: 35,786 km (22,236 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Delayed from April 10. As of 2007 Mar 10 located at 79.96W drifting at 3.741W degrees per day..
2004 October 29 - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2M.
- Ekspress AM-1 - .
Mass: 2,542 kg (5,604 lb). Nation: Russia.
Agency: ILS.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Gals.
USAF Sat Cat: 28463 . COSPAR: 2004-043A. Apogee: 35,792 km (22,240 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.1000 deg. Period: 1,436.10 min.
Russian Satellite Communications Company spacecraft, to be stationed at 40 deg E, providing 28 C, Ku, and L band transponders for a wide range of communications and data services. The Ekspress-AM uses an improved Ekspress-M or 727M bus, first used on the Sesat satellite, while the earlier models used the KAUR-4 MSO-2500 bus. As of 2007 Mar 10 located at 39.98E drifting at 0.006W degrees per day.
2005 March 29 - .
22:31 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2M.
- Ekspress AM-2 - .
Mass: 2,600 kg (5,700 lb). Nation: Russia.
Agency: Svyaz.
Manufacturer: Cannes,
Reshetnev Design Bureau.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Gals.
USAF Sat Cat: 28629 . COSPAR: 2005-010A. Apogee: 35,893 km (22,302 mi). Perigee: 35,773 km (22,228 mi). Inclination: 0.1000 deg. Period: 1,438.50 min. Delayed from December 2004, then moved up from March 31, 2005. Communications payload of C, Ku and L band transponders. It was to be stationed at 80 deg E. As of 2007 Mar 10 located at 80.01E drifting at 0.008W degrees per day..
2005 June 24 - .
19:41 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-K/DM-2.
- Ekspress AM-3 - .
Payload: Ekspress AM. Mass: 2,600 kg (5,700 lb). Nation: Russia.
Agency: Svyaz.
Manufacturer: Cannes,
Reshetnev Design Bureau.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Gals.
USAF Sat Cat: 28707 . COSPAR: 2005-023A. Apogee: 35,791 km (22,239 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Delayed from April 2005. Satellite built by NPO PM with Alcatel C-, Ku- and L-band transponders.Stationed over 80 deg E longitude. As of 2007 Mar 11 located at 139.98E drifting at 0.015W degrees per day..
2008 January 28 - .
00:18 GMT - .
Launch Site: Baikonur.
LV Family: Proton.
Launch Vehicle: Proton-M/Briz-M.
- Ekspress AM-33 - .
Mass: 2,579 kg (5,685 lb). Nation: Russia.
Agency: Svyaz.
Manufacturer: Cannes,
Reshetnev Design Bureau.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Gals.
USAF Sat Cat: 32478 . COSPAR: 2008-003A. Apogee: 35,795 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.0300 deg. Period: 1,436.12 min. Stationed at 96.5 degrees east longitude to provide Internet, video, radio, and data services for at a planned 12 year life. The satellite also was earmarked to provide mobile communications for the Russian president and other top government officials..
2009 February 11 - .
00:03 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC200/39.
LV Family: Proton.
Launch Vehicle: Proton-M/Briz-M.
- Ekspress AM-44 - .
Mass: 3,672 kg (8,095 lb). Nation: Russia.
Agency: Chelomei Design Bureau.
Class: Communications.
Type: Civilian communications satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Gals.
USAF Sat Cat: 33595 . COSPAR: 2009-007A. Apogee: 35,790 km (22,230 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.0000 deg. Period: 1,436.10 min.
2014 April 16 - .
16:20 GMT - .
Launch Site: Baikonur.
Launch Complex: Baikonur LC31.
LV Family: R-7.
Launch Vehicle: Soyuz-U.
- Egyptsat-2 - .
Mass: 1,050 kg (2,310 lb). Nation: Egypt.
Class: Surveillance.
Type: Surveillance satellite. Spacecraft Bus: KAUR-4.
Spacecraft: Yamal.
USAF Sat Cat: 39678 . COSPAR: 2014-021A. Apogee: 710 km (440 mi). Perigee: 649 km (403 mi). Inclination: 51.6200 deg. Period: 98.34 min. Bult by RKK Energia for Egypt's National Authority for Remote Sensing and Space Science using the 559GK bus; carried a 1-meter resolution imager..
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