LEMUR 2 THEODOSIA
Satellite information LEMUR 2 THEODOSIA
| Spacetrack Directory Name | LEMUR 2 THEODOSIA |
| Orbit launches |
2019-12-11 |
| Country/organisation of origin | USA (US) |
| Starting point | SRILR (Satish Dhawan Space Centre, India) |
| WWW | Here |
| Categories | |
| Perigee | 561 km/h |
| Apogee | 570 km |
| Height LEMUR 2 THEODOSIA | 443.39 km |
Additional information LEMUR 2 THEODOSIA
Weather data for government and commercial customers. Measuring signals from GPS satellites as those signals pass through the atmosphere. STRATOS imaging payload and the SENSE AIS payload. The SENSE payload enables tracking shipos worldwide by receiving their AIS signals. GPS radio occultation, provides profiles of temperature, pressure, and humidity in the atmosphere that can be incorporated into weather forecasting models.
satellite LEMUR 2 THEODOSIA Date of exalting 11.12.2019y. Average height of ISS LEMUR 2 THEODOSIA hundred 443.39 km. Average velocity LEMUR 2 THEODOSIA is 27536.56 km/h. Inclination LEMUR 2 THEODOSIA satellite 36.96°.Average orbit height LEMUR 2 THEODOSIA
Average velocity LEMUR 2 THEODOSIA
Average inclination LEMUR 2 THEODOSIA
Photos LEMUR 2 THEODOSIA Photos: 17
