ITOS-E
| Mission type | NOAA[1] |
|---|---|
| Mission duration | Launch failure |
| Spacecraft properties | |
| Manufacturer | RCA Astro |
| Launch mass | 747 kilograms (1,647 lb) |
| Start of mission | |
| Launch date | July 16, 1973, 00:00 UTC SLC-2W |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Sun-synchronous |
| Epoch | Planned |
ITOS-E was a
Delta rocket
, but failed to achieve orbit.
References
- ^ "NASA/NSSDC ITOS-E1 spacecraft details". Retrieved June 7, 2018.
- ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved June 7, 2018.
- ^ Wade, Mark. "ITOS". Encyclopedia Astronautica. Archived from the original on June 21, 2002. Retrieved June 7, 2018.
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