DECAYED
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LEMUR 2 TINYKEV, 43883 (Decayed)

Orbit data source: Space-Track

LEMUR 2 TINYKEV, 43883 was a payload satellite owned by Spire/Lux (US) in LEO that was launched on Thu, 27 Dec 2018 UTC via a SOYUZ-2-1A launch vehicle from the Vostochny Cosmodrome (VOSTO). 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
43883, 2018-111H
Orbit
Decayed
Last TLE update
6 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)
2018-12-27 (7 years ago)
Launch vehicle
SOYUZ-2-1A
Launch site
Vostochny Cosmodrome (VOSTO)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.124 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 6 months ago
0 LEMUR 2 TINYKEV
1 43883U 18111H   25005.82216436  .14718405  29142-5  27515-3 0  9998
2 43883  97.5154 294.0748 0004925 184.7521 175.3736 16.47433148331180
Epoch: 2025-01-05T19:43Z
TLE epoch observation values (Epoch: 2025-01-05T19:43:55Z)
Latitude
-0.00005°
Longitude
-107.55688°
Altitude
152.565 km
Speed
7.813 km/s
True Right ascension
19h 36m 17s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Visualization observer readout
Orbital elements
Apogee altitude
146.118 km
Perigee altitude
139.695 km
Semi-major axis
6,521.044 km
Eccentricity
0.00049
Inclination
97.5154°
RAAN
294.0748°
Arg. of periapsis
184.7521°
True anomaly
175.37815°
Mean anomaly
175.3736°
Eccentric anomaly
175.37587°
Mean motion
4.12162 °/min
Orbital period
87.34 mins
BSTAR
0.00027515
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