LEMUR 2 THEODOSIA, 44863 (Decayed)
Orbit data source: Space-Track
LEMUR 2 THEODOSIA, 44863 was a payload satellite owned by Spire (US) in LEO that was launched on Wed, 11 Dec 2019 UTC via a PSLV-QL launch vehicle from the Sirharikota (SRI). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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44863 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Decayed Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4.6 kg wet, 4.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.124 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 LEMUR 2 THEODOSIA
1 44863U 19089M 24260.89690453 .05892667 36754-5 10562-2 0 9999
2 44863 36.9501 103.8323 0004555 291.9698 68.0602 16.31444996263206Epoch: 2024-09-16T21:31Z
TLE epoch observation values (Epoch: 2024-09-16T21:31:32.551Z)
Latitude
-0.00001°
Longitude
144.62733°
Altitude
186.615 km
Speed
7.797 km/s
True Right ascension
06h 55m 19s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
16:00:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
194.729 km
Perigee altitude
188.743 km
Semi-major axis
6,569.873 km
Eccentricity
0.00046
Inclination
36.9501°
RAAN
103.8323°
Arg. of periapsis
291.9698°
True anomaly
68.10863°
Mean anomaly
68.0602°
Eccentric anomaly
68.08441°
Mean motion
4.07575 °/min
Orbital period
88.33 mins
BSTAR
0.0010562
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Other satellites on launch #89 in the year 2019 (2019-12-11 UTC)
LEMUR 2 THEODOSIA Visibility
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Authenticating...
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