DECAYED
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LEMUR 2 JINDRA, 46909 (Decayed)

Orbit data source: Space-Track

LEMUR 2 JINDRA, 46909 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). 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
46909, 2020-081E
Orbit
Decayed
Last TLE update
10 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)
2020-11-07 (5 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 10 months ago
0 LEMUR 2 JINDRA
1 46909U 20081E   24243.56434529  .01468094  11570-2  29119-2 0  9994
2 46909  36.8843 340.2867 0013719  50.5912 309.6073 15.98992038210785
Epoch: 2024-08-30T13:32Z
TLE epoch observation values (Epoch: 2024-08-30T13:32:39.433Z)
Latitude
-0.00001°
Longitude
157.88684°
Altitude
270.479 km
Speed
7.751 km/s
True Right ascension
22h 41m 08s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Visualization observer readout
Orbital elements
Apogee altitude
289.396 km
Perigee altitude
271.126 km
Semi-major axis
6,658.398 km
Eccentricity
0.00137
Inclination
36.8843°
RAAN
340.2867°
Arg. of periapsis
50.5912°
True anomaly
Unknown
Mean anomaly
309.6073°
Eccentric anomaly
Unknown
Mean motion
3.99474 °/min
Orbital period
90.12 mins
BSTAR
0.0029119
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LEMUR 2 JINDRA Visibility

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