LEMUR 2 REMY-COLTON, 43884 (Decayed)
Orbit data source: Space-Track
LEMUR 2 REMY-COLTON, 43884 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.
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43884 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated 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)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.124 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 LEMUR 2 REMY-COLTON
1 43884U 18111J 25100.62951284 .20655006 30031-5 44424-3 0 9991
2 43884 97.5720 32.5123 0005642 160.8574 199.2941 16.46601126343630Epoch: 2025-04-10T15:06Z
TLE epoch observation values (Epoch: 2025-04-10T15:06:29.909Z)
Latitude
-0.00006°
Longitude
-33.21145°
Altitude
155.033 km
Speed
7.811 km/s
True Right ascension
02h 10m 02s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
16:32:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
148.789 km
Perigee altitude
141.428 km
Semi-major axis
6,523.245 km
Eccentricity
0.00056
Inclination
97.572°
RAAN
32.5123°
Arg. of periapsis
160.8574°
True anomaly
199.27275°
Mean anomaly
199.2941°
Eccentric anomaly
199.28342°
Mean motion
4.11953 °/min
Orbital period
87.39 mins
BSTAR
0.00044424
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Other satellites on launch #111 in the year 2018 (2018-12-27 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.LEMUR 2 REMY-COLTON Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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