LEMUR 2 PAPPY, 44861 (Decayed)

Orbit data source: Space-Track

LEMUR 2 PAPPY, 44861 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). 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 PAPPY details

Identifier	44861, 2019-089K
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)	2019-12-11 (5 years ago)
Launch vehicle	PSLV-QL
Launch site	Sirharikota (SRI)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 2 Pan, 0.7 m
Radar Cross Section	0.124 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 3 months ago

0 LEMUR 2 PAPPY
1 44861U 19089K   24281.31938788  .03913180  32013-1  43153-2 0  9997
2 44861  36.9369 359.8453 0011361  60.3040 299.8868 16.12538234266181

Epoch: 2024-10-07T07:39Z

Definitive object data (Epoch: 2024-10-07T07:39:55.112Z)

Latitude	-0°
Longitude	-131.58303°
Altitude	235.228 km
Speed	7.77 km/s
True Right ascension	23h 59m 22s
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	250.467 km
Perigee altitude	235.422 km
Semi-major axis	6,621.081 km
Eccentricity	0.0011361
Inclination	36.9369°
RAAN	359.8453°
Arg. of periapsis	60.304°
True anomaly	299.77385°
Mean anomaly	299.8868°
Eccentric anomaly	299.83033°
Mean motion	4.02856 °/min
BSTAR	0.0043153
Orbital period	89.36 mins