Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Ariane 2
Part of Ariane Family
Ariane 2 V23
Ariane 2 V23
Ariane 2 V23 - COSPAR 1988-040
Basic three stage vehicle without solid rocket motor strap-ons. Payload to geosynchronous transfer orbit was 2,175 kg.

Status: Retired 1989. First Launch: 1986-05-31. Last Launch: 1989-04-02. Number: 6 . Payload: 2,175 kg (4,795 lb). Thrust: 2,689.00 kN (604,511 lbf). Gross mass: 217,000 kg (478,000 lb). Height: 49.00 m (160.00 ft). Diameter: 3.80 m (12.40 ft).

LEO Payload: 2,175 kg (4,795 lb). Payload: 2,175 kg (4,795 lb) to a GTO.


More at: Ariane 2.

Family: orbital launch vehicle. Country: France. Spacecraft: Intelsat 5A, Spacebus 300. Projects: Intelsat, TDF, TELE, TVSAT. Launch Sites: Kourou, Kourou ELA1, Kourou ELA2. Stages: Ariane 1-2, Ariane 2-1, Ariane 2-3 H10. Agency: Les Mureaux.

1986 May 31 - . 00:53 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 2. FAILURE: Third stage ignition failure. Destroyed by range safety.. Failed Stage: U.
1987 November 21 - . 02:19 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 2.
  • TVSAT 1 - . Payload: TV-Sat 1. Mass: 2,077 kg (4,579 lb). Nation: Germany. Agency: Bundespost. Program: TVSAT. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 300. Completed Operations Date: 1989-02-01 . USAF Sat Cat: 18570 . COSPAR: 1987-095A. Apogee: 36,151 km (22,463 mi). Perigee: 36,066 km (22,410 mi). Inclination: 4.3000 deg. Period: 1,452.60 min.

    West German communications; solar panel failed to deploy making spacecraft unusable. Because of a malfunction of the solar generator, the satellite is being used only for technical tests. Geostationary position 19 W. Launch by Ariane-2 flight no. 20. Due to a malfunction of the solar generator, TV-SAT 1 was taken out of commission and sen t to a so-called parking orbit beyond the geostationary orbit. Semi-major axis 42485.605 km. Eccentricity 0.00116. Inc 0.716, Arg of perigee 216.66, RA 76.77, Mean anomaly 47.1 Mean drift -4.071 deg/day, E long 350.617, latitude -0.713. Positioned in geosynchronous orbit at 18 deg W in 1988 As of 5 September 2001 located at 76.53 deg W drifting at 4.886 deg W per day. As of 2007 Mar 11 located at 169.62W drifting at 4.874W degrees per day.


1988 May 17 - . 23:58 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 2.
  • Intelsat 5A F-13 - . Mass: 2,013 kg (4,437 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: Intelsat 5. Spacecraft: Intelsat 5A. USAF Sat Cat: 19121 . COSPAR: 1988-040A. Apogee: 35,800 km (22,200 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.1000 deg. Period: 1,436.20 min.

    Replaced Intelsat 5 F-3; 53 deg W. Positioned in geosynchronous orbit at 53 deg W in 1988-1995; 177 deg W in 1995-1999 As of 5 September 2001 located at 177.08 deg W drifting at 0.009 deg W per day. As of 2007 Mar 8 located at 44.56W drifting at 6.109W degrees per day.


1988 October 28 - . 02:17 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 2.
  • TDF-1 - . Payload: TDF 1. Mass: 2,136 kg (4,709 lb). Nation: France. Agency: France Telecom. Program: TDF. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 300. Completed Operations Date: 1996-10-04 . USAF Sat Cat: 19621 . COSPAR: 1988-098A. Apogee: 36,129 km (22,449 mi). Perigee: 36,051 km (22,401 mi). Inclination: 4.8000 deg. Period: 1,451.60 min.

    French DBS; 19 deg W. Direct broadcasting satellite. French registration: TDF-1, 1988-5-B. Positioned in geosynchronous orbit at 19 deg W in 1988-1996 As of 1 September 2001 located at 139.53 deg W drifting at 3.885 deg W per day. As of 2007 Mar 5 located at 16.35W drifting at 3.870W degrees per day.


1989 January 27 - . 01:21 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 2.
  • Intelsat 5A F-15 - . Mass: 1,977 kg (4,358 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: Intelsat 5. Spacecraft: Intelsat 5A. USAF Sat Cat: 19772 . COSPAR: 1989-006A. Apogee: 35,801 km (22,245 mi). Perigee: 35,773 km (22,228 mi). Inclination: 0.0000 deg. Period: 1,436.20 min.

    International communications; 18 deg W. Positioned in geosynchronous orbit at 60 deg E in 1989-1992; 18 deg W in 1992-1996; 22 deg W in 1996-1997; 38 deg W in 1998-1999 As of 5 September 2001 located at 37.72 deg W drifting at 0.020 deg W per day. As of 2007 Mar 9 located at 153.76E drifting at 4.192W degrees per day.


1989 April 2 - . 02:28 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 2.
  • TELE-X - . Payload: Tele X. Mass: 2,142 kg (4,722 lb). Nation: Sweden. Agency: NSAB. Program: TELE. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 300. Completed Operations Date: 1998-01-13 . USAF Sat Cat: 19919 . COSPAR: 1989-027A. Apogee: 36,128 km (22,448 mi). Perigee: 36,061 km (22,407 mi). Inclination: 4.3000 deg. Period: 1,451.80 min.

    TV, business communications for Nordic countries; 5 deg E. High power telecommunications satellite with a dual mission; direct TV broadcasting and data communications. Four active transponders with two redundant; power output 200 W per transponder. Coverage area - East Nordic coverage zone as defined by ITU (WARC -77). Mission period estimated to be 6 to 8 years. Position 5 deg E. Positioned in geosynchronous orbit at 5 deg E in 1989-1998 As of 28 August 2001 located at 138.62 deg W drifting at 3.929 deg W per day. As of 2007 Mar 10 located at 132.37W drifting at 3.933W degrees per day.



Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2017 Mark Wade - Contact
© / Conditions for Use