CERTIFICATE OF RE-ENTRYOrbital Register™ · by Orbital Radar™
Entry no.
2024-1474
LEMUR 2 THEODOSIA
LEMUR 2 THEODOSIA (NORAD 44863) re-entered Earth’s atmosphere on 18 September 2024, after 4 years, 9 months in orbit.
Official date
NORAD number
44863
International designator
2019-089M
Object type
Spacecraft
Country
United States
Launched
11 Dec 2019Sriharikota
Re-entered (UTC)
18 Sep 2024UTC calendar day
Time in orbit
4 years, 9 months1,743 days
How it ended
Re-entered (natural decay)
Latitude range
37.0°N to 37.0°SFinal inclination 37.0°
Mass
5 kg
Operator
Built by
Spire/Glasgow
Bus
Cubesat 3U
Programme
Spire
Where it came down
Latitude band its orbit allowedExact position not recorded
No position was recorded for this re-entry. Its final orbit, inclined at 37.0°, allowed a re-entry anywhere between 37.0°N and 37.0°S.
Life in orbit
4 years, 9 monthsLEMUR 2 THEODOSIA’s lowest and highest points above Earth, week by week, from its tracking history.
Also ended on 18 Sep 2024
11 entriesFrom the same launch
2019-089
Entered in the Orbital Register™, founding volume, September 2026.
Record version 1 · No corrections · orbitalradar.com/register/2024-1474
© 2026 Orbital Radar. Cite this entry by its number; the register itself may not be copied.
Record version 1 · No corrections · orbitalradar.com/register/2024-1474
© 2026 Orbital Radar. Cite this entry by its number; the register itself may not be copied.