Lemur · Payload
LEMUR-2-THEODOSIA
DecayedPayloadLEO
LEMUR-2-THEODOSIA is a Spire Global Inc. payload satellite, part of the Lemur constellation, launched on December 11, 2019 into LEO. It has since re-entered the atmosphere.
Loading…
Launch
- Launch date
- December 11, 2019 at 09:55 AM UTC
- Launch site
- Satish Dhawan / Sriharikota, India
- Launched by
- PSLV-QL →
- Operator
- Indian Space Research Organization
- Mission
- RISAT-2BR1 & others
- Launch record
- View full launch →
Orbit
- Orbit regime
- LEO
- Apoapsis
- 194 km
- Periapsis
- 187 km
- Inclination
- 36.95°
- Orbital period
- 88.3 min
Spacecraft
- Operator
- Spire Global Inc.
- Manufacturer
- Spire Global
- Users
- Commercial
- Launch mass
- 4.6 kg
- Design lifetime
- 3 years
- Detailed purpose
- Meteorology, Automatic Identification System (AIS)
Identity
- COSPAR (Int'l)
- 2019-089M
- NORAD catalog №
- 44863
- Object type
- Payload
- Owner / operator
United States- Constellation
- Lemur
- Status
- Decayed
- Decay / reentry
- September 18, 2024
End of mission
- Last active / ended
- September 18, 2024
- Time in service
- 4.8 years
- Fate
- Reentered Earth's atmosphere and was destroyed.
- Final status
- Decayed