PROMETHEUS 2-3
Satellite information PROMETHEUS 2-3
| Spacetrack Directory Name | PROMETHEUS 2-3 |
| Follow PROMETHEUS 2-3 | PROMETHEUS 2-3 Tracker |
| Pass predictions PROMETHEUS 2-3 | Pass predictions PROMETHEUS 2-3 |
| Orbit launches |
2016-11-11 (7 years ago)
|
| Days in orbit | 2882 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 568 km/h |
| Apogee | 582 km |
| Orbit slope (inclination) | 98.09° |
| Laps per day | 15 |
| Orbit | LEO (Equatorial) |
| Height PROMETHEUS 2-3 | 535.19 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.
satellite PROMETHEUS 2-3 Date of exalting 11.11.2016y. Average height of ISS PROMETHEUS 2-3 hundred 535.19 km. Average velocity PROMETHEUS 2-3 is 27347.46 km/h. Inclination PROMETHEUS 2-3 satellite 98.09°.TLE
Average orbit height PROMETHEUS 2-3
Average velocity PROMETHEUS 2-3
Average inclination PROMETHEUS 2-3
Photos PROMETHEUS 2-3 Photos: 6
