DECAYED
Showing default

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.

Not visible in the next 10 days
Identifier
44863, 2019-089M
Orbit
Decayed
Country
Flag of USUS
Related 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)
2019-12-11 (6 years ago)
Launch vehicle
PSLV-QL
Launch site
Sirharikota (SRI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.124 m², Small (<0.1 m²)

Expand to show TLE details & history
Last 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 16.31444996263206
Epoch: 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
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
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
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|