AS 3000

1978 December 16

00:21 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Thor. Launch Vehicle: Delta 3914.

• Anik B1 (Telesat 4) - . Payload: Anik B1. Mass: 900 kg (1,980 lb). Nation: Canada. Agency: Telesat. Program: Anik. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: AS 3000. Spacecraft: Anik satellite. Completed Operations Date: 1986-12-17 . USAF Sat Cat: 11153 . COSPAR: 1978-116A. Apogee: 35,927 km (22,323 mi). Perigee: 35,900 km (22,300 mi). Inclination: 6.60 deg. Period: 1,442.60 min.

  Longitude 109.0. Function - telecommunications. Operating entity - Telesat Canada. Positioned in geosynchronous orbit over the Americas at 109 deg W in 1978-1986 As of 29 August 2001 located at 59.48 deg E drifting at 1.672 deg W per day. As of 2007 Mar 9 located at 13.64W drifting at 1.622W degrees per day.

1981 November 20

01:37 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Thor. Launch Vehicle: Delta 3910/PAM.

• RCA Satcom 3R - . Payload: Satcom 3R. Mass: 1,078 kg (2,376 lb). Nation: USA. Agency: RCA Amer. Manufacturer: Lockheed. Program: Satcom. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 1991-04-10 . USAF Sat Cat: 12967 . COSPAR: 1981-114A. Apogee: 35,840 km (22,260 mi). Perigee: 35,824 km (22,259 mi). Inclination: 8.20 deg. Period: 1,438.40 min. Positioned in geosynchronous orbit at 131 deg W in 1981-1991 As of 3 September 2001 located at 86.96 deg W drifting at 0.634 deg W per day. As of 2007 Mar 11 located at 140.04W drifting at 0.601W degrees per day..

1982 January 16

01:55 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Thor. Launch Vehicle: Delta 3910/PAM.

• RCA Satcom 4 - . Payload: Satcom 4. Mass: 1,082 kg (2,385 lb). Nation: USA. Agency: RCA Amer. Manufacturer: Lockheed. Program: Satcom. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 1991-12-06 . USAF Sat Cat: 13035 . COSPAR: 1982-004A. Apogee: 35,994 km (22,365 mi). Perigee: 35,964 km (22,346 mi). Inclination: 1.90 deg. Period: 1,446.00 min. Positioned in geosynchronous orbit at 83 deg W in 1982-1987; 82 deg W in 1987-1991 As of 2 September 2001 located at 171.96 deg E drifting at 2.443 deg W per day. As of 2007 Mar 9 located at 101.04W drifting at 2.479W degrees per day..

1982 October 28

01:28 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 3924.

• RCA Satcom 5 - . Payload: Aurora 1. Mass: 590 kg (1,300 lb). Nation: USA. Agency: RCA Alas. Manufacturer: Lockheed. Program: Satcom. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 1992-09-23 . USAF Sat Cat: 13631 . COSPAR: 1982-105A. Apogee: 35,791 km (22,239 mi). Perigee: 35,782 km (22,233 mi). Inclination: 8.10 deg. Period: 1,436.10 min. Positioned in geosynchronous orbit at 143 deg W in 1982-1991; 105 deg W in 1992-2007..

1983 April 11

21:39 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 3924.

• RCA Satcom 6 - . Payload: Satcom 1R. Mass: 2,385 kg (5,258 lb). Nation: USA. Agency: RCA Amer. Manufacturer: Lockheed. Program: Satcom. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 1992-12-27 . USAF Sat Cat: 13984 . COSPAR: 1983-030A. Apogee: 35,953 km (22,340 mi). Perigee: 35,851 km (22,276 mi). Inclination: 7.00 deg. Period: 1,442.00 min. Positioned in geosynchronous orbit at 139 deg W in 1983-1991; 131 deg W in 1991-1992 As of 5 September 2001 located at 148.59 deg W drifting at 1.499 deg W per day. As of 2007 Mar 10 located at 90.26E drifting at 1.535W degrees per day..

1983 September 8

22:52 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 3924.

• RCA Satcom 7 - . Payload: Satcom 2R. Mass: 1,121 kg (2,471 lb). Nation: USA. Agency: RCA Amer. Manufacturer: Lockheed. Program: Satcom. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 1995-03-05 . USAF Sat Cat: 14328 . COSPAR: 1983-094A. Apogee: 36,095 km (22,428 mi). Perigee: 35,963 km (22,346 mi). Inclination: 5.70 deg. Period: 1,448.50 min. Positioned in geosynchronous orbit at 72 deg W in 1983-1995 As of 4 September 2001 located at 143.00 deg E drifting at 3.084 deg W per day. As of 2007 Mar 10 located at 40.27E drifting at 3.104W degrees per day..

1984 January 23

07:58 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima N. LV Family: Thor. Launch Vehicle: N-2.

• Yuri 2A - . Payload: BS-2a. Mass: 670 kg (1,470 lb). Nation: Japan. Agency: NASDA. Manufacturer: Lockheed. Program: BS. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 1989-07-01 . USAF Sat Cat: 14659 . COSPAR: 1984-005A. Apogee: 36,191 km (22,488 mi). Perigee: 36,072 km (22,414 mi). Inclination: 4.90 deg. Period: 1,453.80 min.

  TV. BS-2a (Yuri-2a). Domestic satellite broadcasting; development of broadcasting satellite technology. Launch 0758 GMT. N launch vehicle flight no 12. Launching organization NASDA. Positioned in geosynchronous orbit at 110 deg E in 1984-1985; 108 deg E in 1985-1987; 110 deg E in 1987-1988 As of 28 August 2001 located at 69.57 deg E drifting at 4.403 deg W per day. As of 2007 Mar 10 located at 153.52W drifting at 4.395W degrees per day.

1984 May 23

01:33 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 1.

• Spacenet F1 - . Mass: 705 kg (1,554 lb). Nation: USA. Agency: GTE. Manufacturer: Lockheed. Program: GTE. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. USAF Sat Cat: 14985 . COSPAR: 1984-049A. Apogee: 35,897 km (22,305 mi). Perigee: 35,840 km (22,260 mi). Inclination: 4.90 deg. Period: 1,440.30 min.

  Stationed at 120 deg W. C, Ku band communications satellite. Positioned in geosynchronous orbit at 120 deg W in 1984-1993; 115 deg E in 1993-on. As of 2 September 2001 located at 165.12 deg E drifting at 0.985 deg W per day. As of 2007 Mar 10 located at 109.23W drifting at 1.077W degrees per day.

1984 November 10

01:14 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 3.

• Spacenet F2 - . Mass: 705 kg (1,554 lb). Nation: USA. Agency: GTE. Manufacturer: Lockheed. Program: GTE. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 1998-06-02 . USAF Sat Cat: 15385 . COSPAR: 1984-114A. Apogee: 35,962 km (22,345 mi). Perigee: 35,904 km (22,309 mi). Inclination: 4.20 deg. Period: 1,443.60 min.

  Stationed at 68 deg W. C, Ku band communications satellite. Positioned in geosynchronous orbit at 69 deg W in 1984-1997; 115 deg E in 1997-1998 As of 5 September 2001 located at 65.20 deg E drifting at 1.887 deg W per day. As of 2007 Mar 9 located at 64.76W drifting at 1.866W degrees per day.

1985 May 8

01:15 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 3.

• GStar 1 - . Mass: 705 kg (1,554 lb). Nation: USA. Agency: GTE. Manufacturer: Lockheed. Program: GTE. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 1997-01-01 . USAF Sat Cat: 15677 . COSPAR: 1985-035A. Apogee: 35,791 km (22,239 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.10 deg. Period: 1,436.10 min.

  Stationed at 103 deg W. Ku band communications satellite. Positioned in geosynchronous orbit at 103 deg W in 1985-1996; 105 deg W in 1997-1999 As of 5 September 2001 located at 105.33 deg W drifting at 0.011 deg W per day. As of 2007 Mar 9 located at 105.07W drifting at 0.006W degrees per day.

1985 August 27

10:58 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. Launch Platform: MLP1. LV Family: Shuttle. Launch Vehicle: Space Shuttle.

• ASC-1 - . Mass: 1,271 kg (2,802 lb). Nation: USA. Agency: new. Program: GTE. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: AS 3000. Spacecraft: ASC. Completed Operations Date: 1994-08-01 . USAF Sat Cat: 15994 . COSPAR: 1985-076C. Apogee: 35,796 km (22,242 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.00 deg. Period: 1,436.10 min.

  Released by STS 51I 8/27/85; stationed at 81 deg E. C, Ku band communications satellite. Positioned in geosynchronous orbit at 128 deg W in 1985-1994 As of 5 September 2001 located at 99.97 deg W drifting at 0.156 deg W per day. As of 2007 Mar 10 located at 119.21W drifting at 0.126W degrees per day.

1985 September 12

23:26 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 3. FAILURE: Geosynchronous orbit injection failure. Third stage igniter cartridge failure was determined to be the most likely cause..

• Spacenet F3 - . Mass: 600 kg (1,320 lb). Nation: USA. Agency: Arianespace. Manufacturer: Lockheed. Program: GTE. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000.

1986 February 12

07:55 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima N. LV Family: Thor. Launch Vehicle: N-2.

• Yuri 2B - . Payload: BS-2b. Mass: 677 kg (1,492 lb). Nation: Japan. Agency: NASDA. Manufacturer: Lockheed. Program: BS. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 1991-10-24 . USAF Sat Cat: 16597 . COSPAR: 1986-016A. Apogee: 36,135 km (22,453 mi). Perigee: 35,996 km (22,366 mi). Inclination: 2.70 deg. Period: 1,450.40 min.

  Stationed at 117 deg E. BS-2b (Yuri-2b). Domestic satellite broadcasting; development of broadcasting satellite technology. Launching organization NASDA. N launch vehicle flight no 14. Launch time 0755 GMT. Positioned in geosynchronous orbit at 110 deg E in 1986-1991 As of 5 September 2001 located at 13.60 deg W drifting at 3.524 deg W per day. As of 2007 Mar 11 located at 77.04E drifting at 3.551W degrees per day.

1986 March 28

23:30 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 3.

• GStar 2 - . Payload: SBTS-2. Mass: 1,140 kg (2,510 lb). Nation: USA. Agency: GTE. Manufacturer: Lockheed. Program: GTE. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 1997-08-20 . USAF Sat Cat: 16649 . COSPAR: 1986-026A. Apogee: 35,943 km (22,333 mi). Perigee: 35,902 km (22,308 mi). Inclination: 5.60 deg. Period: 1,443.10 min.

  Ku band communications satellite. Stationed at 70 degrees W. Positioned in geosynchronous orbit at 105 deg W in 1986-1992; 125 deg W in 1992-1997 As of 5 September 2001 located at 148.11 deg W drifting at 1.728 deg W per day. As of 2007 Mar 10 located at 2.39W drifting at 1.699W degrees per day.

1988 March 11

23:28 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 3.

• Spacenet F3R - . Payload: Spacenet 3R. Mass: 1,212 kg (2,672 lb). Nation: USA. Agency: France Telecom. Manufacturer: Lockheed. Program: GTE. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 1999-12-01 . USAF Sat Cat: 18951 . COSPAR: 1988-018A. Apogee: 35,980 km (22,350 mi). Perigee: 35,935 km (22,328 mi). Inclination: 2.40 deg. Period: 1,444.90 min.

  US domestic communications; 87 deg W. C, Ku band communications satellite. Positioned in geosynchronous orbit at 87 deg W in 1988-1997; 83 deg W in 1997-1999 As of 2 September 2001 located at 107.85 deg W drifting at 2.220 deg W per day. As of 2007 Mar 9 located at 153.60E drifting at 2.179W degrees per day.

1988 June 15

11:19 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44LP.

• Panamsat 1 - . Payload: PAS 1. Mass: 1,220 kg (2,680 lb). Nation: USA. Agency: Panamsat. Program: Panamsat. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: AS 3000. Spacecraft: ASC. USAF Sat Cat: 19217 . COSPAR: 1988-051C. Apogee: 36,043 km (22,396 mi). Perigee: 36,028 km (22,386 mi). Inclination: 1.20 deg. Period: 1,448.90 min. Stationed at 45 deg W. Positioned in geosynchronous orbit at 45 deg W in 1988-1999 As of 5 September 2001 located at 139.29 deg E drifting at 3.164 deg W per day. As of 2007 Mar 11 located at 114.72W drifting at 3.187W degrees per day..

1988 September 8

23:00 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 3.

• GStar 3 - . Mass: 1,270 kg (2,790 lb). Nation: USA. Agency: GTE. Manufacturer: Lockheed. Program: GTE. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 1998-01-01 . USAF Sat Cat: 19483 . COSPAR: 1988-081A. Apogee: 35,806 km (22,248 mi). Perigee: 35,769 km (22,225 mi). Inclination: 5.30 deg. Period: 1,436.20 min.

  AKM malfunctioned, but orbit achieved using on-board propulsion system. Ku band communications satellite. Positioned in geosynchronous orbit at 93 deg W in 1989-1996; 105 deg W in 1996-1999 As of 5 September 2001 located at 105.39 deg W drifting at 0.005 deg W per day. As of 2007 Mar 9 located at 105.31W drifting at 0.004W degrees per day.

1990 August 28

09:05 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima N. LV Family: Thor. Launch Vehicle: H-1.

• Yuri 3A - . Payload: BS-3a. Mass: 1,115 kg (2,458 lb). Nation: Japan. Manufacturer: Lockheed. Program: BS. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 1998-04-20 . USAF Sat Cat: 20771 . COSPAR: 1990-077A. Apogee: 36,245 km (22,521 mi). Perigee: 36,157 km (22,466 mi). Inclination: 3.50 deg. Period: 1,457.30 min.

  Japanese DBS; 110 deg E. Continuation of broadcasting services by BS-2; accommodations to increasing and diversifying demands for broadcasting; establishment of common technology necessary for broadcasting satellite. Launching organization NASDA. Launch time 0905 GMT. BS-3a 'Yuri -3a'. Positioned in geosynchronous orbit at 110 deg E in 1990-1998 As of 2 September 2001 located at 84.62 deg E drifting at 5.278 deg W per day. As of 2007 Mar 10 located at 83.70W drifting at 5.275W degrees per day.

1990 November 20

23:11 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 42P.

• Satcom C1 - . Payload: Satcom C1. Mass: 1,169 kg (2,577 lb). Nation: USA. Agency: GE Americom. Manufacturer: Lockheed. Program: Satcom. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. USAF Sat Cat: 20945 . COSPAR: 1990-100A. Apogee: 35,794 km (22,241 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.10 deg. Period: 1,436.10 min.

  Stationed at 137 deg W. Positioned in geosynchronous orbit at 137 deg W in 1990-1991; 139 deg W in 1991; 137 deg W in 1991-1999 As of 5 September 2001 located at 78.98 deg W drifting at 0.013 deg W per day. As of 2007 Mar 9 located at 151.83E drifting at 3.912W degrees per day.

• GStar 4 - . Mass: 1,295 kg (2,854 lb). Nation: USA. Agency: GTE. Manufacturer: Lockheed. Program: GTE. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. USAF Sat Cat: 20946 . COSPAR: 1990-100B. Apogee: 35,790 km (22,230 mi). Perigee: 35,785 km (22,235 mi). Inclination: 0.00 deg. Period: 1,436.10 min.

  Stationed at 125 deg W. Ku band communications satellite. Positioned in geosynchronous orbit at 125 deg W in 1990-1992; 105 deg W in 1992-1999 As of 6 September 2001 located at 104.95 deg W drifting at 0.005 deg W per day. As of 2007 Mar 10 located at 74.47W drifting at 4.077W degrees per day.

1991 April 13

00:09 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 7925.

• ASC-2 / Spacenet F4 - . Mass: 1,350 kg (2,970 lb). Nation: USA. Agency: Contel. Program: GTE. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: AS 3000. Spacecraft: ASC. USAF Sat Cat: 21227 . COSPAR: 1991-028A. Apogee: 35,794 km (22,241 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.00 deg. Period: 1,436.20 min.

  Commercial business communications; stationed at 101 deg W. C, Ku band communications satellite. Positioned in geosynchronous orbit at 101 deg W in 1991-1999; 81 deg W in 2000. As of 6 September 2001 located at 172.04 deg E drifting at 0.007 deg W per day. As of 2007 Mar 9 located at 34.51E drifting at 2.539W degrees per day.

1991 April 18

23:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas I. FAILURE: RL-10 Centaur engine turbopump failed at T+361 seconds; destroyed by range safety.. Failed Stage: U.

• Yuri 3H - . Payload: BS-3H. Mass: 600 kg (1,320 lb). Nation: Japan. Agency: TSCJ. Manufacturer: Lockheed. Program: BS. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Decay Date: 1991-04-18 . Apogee: 175 km (108 mi).

1991 May 29

22:55 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 7925.

• Aurora 2 - . Payload: Satcom-C 5. Mass: 1,336 kg (2,945 lb). Nation: USA. Agency: GE. Manufacturer: Lockheed. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. USAF Sat Cat: 21392 . COSPAR: 1991-037A. Apogee: 36,161 km (22,469 mi). Perigee: 36,125 km (22,446 mi). Inclination: 1.20 deg. Period: 1,454.40 min.

  Stationed at 139 deg W. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). Positioned in geosynchronous orbit at 139 deg W in 1991-1999 As of 30 August 2001 located at 148.31 deg E drifting at 4.531 deg W per day. As of 2007 Mar 9 located at 2.15E drifting at 4.534W degrees per day.

1991 August 25

08:40 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima N. LV Family: Thor. Launch Vehicle: H-1.

• Yuri 3B - . Payload: BS-3b. Mass: 1,115 kg (2,458 lb). Nation: Japan. Manufacturer: Lockheed. Program: BS. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 1999-04-05 . USAF Sat Cat: 21668 . COSPAR: 1991-060A. Apogee: 36,244 km (22,520 mi). Perigee: 36,171 km (22,475 mi). Inclination: 3.20 deg. Period: 1,457.70 min. TV; 110 deg E. Positioned in geosynchronous orbit at 110 deg E in 1991-1999 As of 3 September 2001 located at 91.59 deg E drifting at 5.350 deg W per day. As of 2007 Mar 9 located at 152.69E drifting at 5.334W degrees per day..

1992 August 31

10:41 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 7925.

• Satcom C4 - . Mass: 2,000 kg (4,400 lb). Nation: USA. Agency: GE Americom. Manufacturer: Lockheed. Program: Satcom. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. USAF Sat Cat: 22096 . COSPAR: 1992-057A. Apogee: 35,789 km (22,238 mi). Perigee: 35,786 km (22,236 mi). Inclination: 0.10 deg. Period: 1,436.20 min. Stationed at 135 deg W. Positioned in geosynchronous orbit at 135 deg W in 1992-1999 As of 3 September 2001 located at 135.00 deg W drifting at 0.002 deg E per day. As of 2007 Mar 10 located at 164.40W drifting at 4.518W degrees per day..

1992 September 10

23:04 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44LP.

• Satcom C3 - . Mass: 1,375 kg (3,031 lb). Nation: USA. Agency: GE Americom. Manufacturer: Lockheed. Program: Satcom. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. USAF Sat Cat: 22117 . COSPAR: 1992-060B. Apogee: 35,789 km (22,238 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Stationed at 131 deg W. Positioned in geosynchronous orbit at 143 deg W in 1992; 131 deg W in 1992-1999 As of 4 September 2001 located at 130.93 deg W drifting at 0.000 deg W per day. As of 2007 Mar 11 located at 79.06W drifting at 0.008W degrees per day..

1994 July 8

23:05 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L.

• Yuri 3N - . Payload: BS-3N. Mass: 1,210 kg (2,660 lb). Nation: Japan. Agency: NHK. Manufacturer: Lockheed. Program: BS. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. USAF Sat Cat: 23176 . COSPAR: 1994-040B. Apogee: 35,797 km (22,243 mi). Perigee: 35,777 km (22,230 mi). Inclination: 0.0500 deg. Period: 1,436.15 min. Stationed at 109.67 deg E. Positioned in geosynchronous orbit at 109 deg E in 1994-1999 As of 5 September 2001 located at 109.71 deg E drifting at 0.013 deg W per day. As of 2007 Mar 11 located at 109.92E drifting at 0.008W degrees per day..

1995 August 5

11:10 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 7925. FAILURE: Partial Failure.. Failed Stage: U.

• Mugunghwa 1 - . Payload: Koreasat 1. Mass: 1,459 kg (3,216 lb). Nation: Korea South. Agency: KT. Manufacturer: Lockheed. Program: Koreasat. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. USAF Sat Cat: 23639 . COSPAR: 1995-041A. Apogee: 35,796 km (22,242 mi). Perigee: 35,776 km (22,230 mi). Inclination: 2.70 deg. Period: 1,436.10 min.

  15 Ku-band transponders; boosted into geosynch orbit by satellite thrusters following Delta failure that left satellite in LEO; unplanned use of satellite propellant cut usable satellite lifetime by approx. 50 percent. Stationed at 116.0 deg E. Stage 1 SRM failure Positioned in geosynchronous orbit at 116 deg E in 1995-1999 As of 5 September 2001 located at 47.22 deg E drifting at 0.022 deg E per day. As of 2007 Mar 9 located at 152.88E drifting at 2.155W degrees per day.

1996 January 14

11:10 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 7925.

• Koreasat 2 - . Mass: 600 kg (1,320 lb). Nation: Korea South. Agency: KT. Manufacturer: Lockheed. Program: Koreasat. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 3000. Completed Operations Date: 2000-04-08 . USAF Sat Cat: 23768 . COSPAR: 1996-003A. Apogee: 35,792 km (22,240 mi). Perigee: 35,782 km (22,233 mi). Inclination: 0.00 deg. Period: 1,436.20 min. Geostationary at 116.0E. Positioned in geosynchronous orbit at 116 deg E in 1996-2000 As of 5 September 2001 located at 113.02 deg E drifting at 0.017 deg W per day. As of 2007 Mar 11 located at 116.35E drifting at 0.013W degrees per day..