Post-launch separation of Vela 5A and 5B
| |
| Operator | USAF |
|---|---|
| COSPAR ID | 1969-046D[1] |
| SATCAT no. | 3954 |
| Spacecraft properties | |
| Manufacturer | TRW |
| Launch mass | 259 kilograms (571 lb) |
| Power | 120 W |
| Start of mission | |
| Launch date | May 23, 1969, 07:57:01 (1969-05-23UTC07:57:01Z) UTC |
| Rocket | Titan III-C 15 |
| Launch site | Cape Canaveral LC-41 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Highly Elliptical |
| Semi-major axis | 117,689 kilometres (73,129 mi) |
| Perigee altitude | 29,122.4 kilometres (18,095.8 mi) |
| Apogee altitude | 193,514.6 kilometres (120,244.4 mi) |
| Inclination | 42° |
| Period | 6,696.8 minutes (111.613 h) |
|
← Vela 4B
Vela 5B →
| |
Vela 5A (also known Vela 9 and OPS 6909[2]) was an American reconnaissance satellite to detect explosions and nuclear tests on land and in space. It was released together with Vela 5B, OV5 5, OV5 6 and OV5 9.[3]
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