| Mission type | Technology |
|---|---|
| Operator | AFRL |
| COSPAR ID | 2000-042A |
| SATCAT no. | 26414 |
| Mission duration | 2 years, 4 months |
| Spacecraft properties | |
| Manufacturer | Spectrum Astro |
| Launch mass | 130 kilograms (290 lb) |
| Power | 330 watts |
| Start of mission | |
| Launch date | July 19, 2000 |
| Rocket | Minotaur I |
| Launch site | Vandenberg SLC-8 |
| Contractor | Orbital Sciences |
| End of mission | |
| Decay date | 12 November 2002 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Eccentricity | 0.00266 |
| Perigee altitude | 548.0 kilometers (340.5 mi) |
| Apogee altitude | 585.0 kilometers (363.5 mi) |
| Inclination | 97.8 degrees |
| Period | 96.0 minutes |
| Epoch | 19 September 2000, 16:09:00 UTC[1] |
| Instruments | |
| Fourier Transform Hyperspectral Imager | |
MightySat-2.1,[2] also known as P99-1 or Sindri was a small spacecraft developed by the Air Force Research Laboratory[3] to test advanced technologies in imaging, communications, and spacecraft bus components in space.
- ^ "NASA - NSSDCA - Spacecraft - Trajectory Details". nssdc.gsfc.nasa.gov. Retrieved 2018-05-02.
- ^ Krebs, Gunter. "Mightysat-2 (P99-1)". Gunter's Space Page. Retrieved 10 July 2013.
- ^ "MightySat II.1 Datasheet" (PDF). General Dynamics. Archived from the original (PDF) on 2007-10-20. Retrieved 2008-08-01.