DECAYED
Showing default

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
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, Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 months ago

TLE from 11 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
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
08:30:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
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
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
|