LEMUR 2 OZARAK, 46908 (Decayed)

Orbit data source: Space-Track

LEMUR 2 OZARAK, 46908 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 OZARAK details

Identifier	46908, 2020-081D
Orbit	Decayed
Last TLE update	2 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 2 months ago

0 LEMUR 2 OZARAK
1 46908U 20081D   24288.74241146  .07682509  36624-5  17104-2 0  9999
2 46908  36.8706  76.1351 0009808 337.4116  22.6234 16.29058783217527

Epoch: 2024-10-14T17:49Z

Definitive object data (Epoch: 2024-10-14T17:49:04.35Z)

Latitude	0.00004°
Longitude	145.10185°
Altitude	188.186 km
Speed	7.799 km/s
True Right ascension	05h 04m 32s
True Declination	0° 00' 00"
Sunlit	Object was in full shadow 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	204.608 km
Perigee altitude	191.707 km
Semi-major axis	6,576.295 km
Eccentricity	0.0009808
Inclination	36.8706°
RAAN	76.1351°
Arg. of periapsis	337.4116°
True anomaly	22.66668°
Mean anomaly	22.6234°
Eccentric anomaly	22.64504°
Mean motion	4.06978 °/min
BSTAR	0.0017104
Orbital period	88.46 mins