PROMETHEUS 2-3
Satellite information PROMETHEUS 2-3 - Prometheus 2.3
| Spacetrack Directory Name | PROMETHEUS 2-3 |
| Alternative name | Prometheus 2.3 |
| Orbit launches |
2016-11-11 |
| Deorbitation date |
2025-12-03 |
| Days in orbit | 3309 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Type | Satellite |
| Perigee | 568 km |
| Apogee | 582 km |
Additional information PROMETHEUS 2-3
Improving from lessons learned on Block 1. Replacing single coil with 3 torque rods, increasing momentum wheel storage, adding star field sensor, adding GPS receiver. Possibility to add 1.5U payload at the end of the satellite.
Average velocity PROMETHEUS 2-3
Average inclination PROMETHEUS 2-3
Mean right ascension of the ascending node (RAAN) PROMETHEUS 2-3
Mean argument of perigee PROMETHEUS 2-3
Mean semi-major axis of the orbit PROMETHEUS 2-3
Mean orbital eccentricity PROMETHEUS 2-3
Photos PROMETHEUS 2-3 Photos: 6
ISS
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