DECAYED
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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). 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
44861, 2019-089K
Orbit
Decayed
Last TLE update
9 months ago
Origin
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, Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 9 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
TLE epoch observation values (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 epoch
Visualization orbit readout
Visualization observer readout
Orbital elements
Apogee altitude
250.467 km
Perigee altitude
235.422 km
Semi-major axis
6,621.081 km
Eccentricity
0.00114
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
Orbital period
89.36 mins
BSTAR
0.0043153
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