LEMUR 2 NATALIEMURRAY, 43887 (Decayed)
Orbit data source: Space-Track
LEMUR 2 NATALIEMURRAY, 43887 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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43887 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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 LEMUR 2 NATALIEMURRAY
1 43887U 18111M 25091.81892129 .13621562 27586-5 12281-2 0 9994
2 43887 97.5592 22.9286 0008671 203.5320 156.5583 16.38996519344231Epoch: 2025-04-01T19:39Z
TLE epoch observation values (Epoch: 2025-04-01T19:39:14.799Z)
Latitude
-0.00001°
Longitude
-102.29806°
Altitude
176.928 km
Speed
7.797 km/s
True Right ascension
01h 31m 42s
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
23:45:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
170.963 km
Perigee altitude
159.616 km
Semi-major axis
6,543.426 km
Eccentricity
0.00087
Inclination
97.5592°
RAAN
22.9286°
Arg. of periapsis
203.532°
True anomaly
156.59779°
Mean anomaly
156.5583°
Eccentric anomaly
156.57805°
Mean motion
4.10049 °/min
Orbital period
87.79 mins
BSTAR
0.0012281
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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 NATALIEMURRAY 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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