LEMUR 2 WALLACE, 46910 (Decayed)

Orbit data source: Space-Track

LEMUR 2 WALLACE, 46910 was a payload satellite owned by Spire (US) in LEO that was launched on Sat, 07 Nov 2020 UTC via a PSLV-DL launch vehicle from the Sirharikota (SRI). Payloads include a variety of satellites, spacecraft, and rockets 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

LEMUR 2 WALLACE details

Identifier	46910, 2020-081F
Orbit	Decayed
Last TLE update	3 months ago
Origin	Spire (US)
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)	2020-11-07 (4 years ago)
Launch vehicle	PSLV-DL
Launch site	Sirharikota (SRI)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 2 Pan, 0.7 m
Radar Cross Section	0.124 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 3 months ago

0 LEMUR 2 WALLACE
1 46910U 20081F   24257.25337996  .16937571  35775-5  10952-2 0  9995
2 46910  36.8866 257.7017 0007599 143.7804 205.6401 16.40543218212844

Epoch: 2024-09-13T06:04Z

Definitive object data (Epoch: 2024-09-13T06:04:52.028Z)

Latitude	-6.43421°
Longitude	165.16423°
Altitude	168.958 km
Speed	7.804 km/s
True Right ascension	16h 36m 26s
True Declination	-6° 23' 33"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	172.431 km
Perigee altitude	162.483 km
Semi-major axis	6,545.594 km
Eccentricity	0.0007599
Inclination	36.8866°
RAAN	257.7017°
Arg. of periapsis	143.7804°
True anomaly	205.60245°
Mean anomaly	205.6401°
Eccentric anomaly	205.62127°
Mean motion	4.09845 °/min
BSTAR	0.0010952
Orbital period	87.84 mins