DECAYED
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LEMUR 2 CHRISTINAHOLT, 43882 (Decayed)

Orbit data source: Space-Track

LEMUR 2 CHRISTINAHOLT, 43882 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
43882, 2018-111G
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)
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, 0.5 m
Radar Cross Section
0.124 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 8 months ago

TLE from 8 months ago
0 LEMUR 2 CHRISTINAHOLT
1 43882U 18111G   25041.19253388  .08539685  26074-5  22548-2 0  9999
2 43882  97.5569 330.2250 0008341 134.1300 226.0680 16.28410585336445
Epoch: 2025-02-10T04:37Z
TLE epoch observation values (Epoch: 2025-02-10T04:37:14.927Z)
Latitude
-0.00003°
Longitude
120.39757°
Altitude
203.854 km
Speed
7.782 km/s
True Right ascension
22h 00m 54s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
10:38:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
199.126 km
Perigee altitude
188.163 km
Semi-major axis
6,571.781 km
Eccentricity
0.00083
Inclination
97.5569°
RAAN
330.225°
Arg. of periapsis
134.13°
True anomaly
225.99922°
Mean anomaly
226.068°
Eccentric anomaly
226.0336°
Mean motion
4.07398 °/min
Orbital period
88.37 mins
BSTAR
0.0022548
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Computing Atmospheric mass density...

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