LEMUR 2 THENICKMOLO, 43185
Orbit data source: Space-Track
LEMUR 2 THENICKMOLO, 43185 is a payload satellite owned by Spire (US) in SSO that was launched on Thu, 01 Feb 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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43185 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Spire/Glasgow
Mission
Operational 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, 0.3 m
Radar Cross Section
0.124 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 LEMUR 2 THENICKMOLO
1 43185U 18014F 25256.73697541 .00464038 81745-4 16866-2 0 9990
2 43185 97.5556 181.1874 0009039 137.0857 223.1121 15.88417857418540Epoch: 2025-09-13T17:41Z
TLE epoch observation values (Epoch: 2025-09-13T17:41:14.675Z)
Latitude
-0.00006°
Longitude
-77.08978°
Altitude
314.311 km
Speed
7.717 km/s
True Right ascension
12h 04m 44s
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
00:46:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
309.64 km
Perigee altitude
297.56 km
Semi-major axis
6,681.737 km
Eccentricity
0.0009
Inclination
97.5556°
RAAN
181.1874°
Arg. of periapsis
137.0857°
True anomaly
223.04137°
Mean anomaly
223.1121°
Eccentric anomaly
223.07673°
Mean motion
3.97383 °/min
Orbital period
90.59 mins
BSTAR
0.0016866
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Other satellites on launch #14 in the year 2018 (2018-02-01 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 THENICKMOLO Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-14 19:30:48.050Z | 200.101° SSW | 2025-09-14 19:32:48.050Z | 258.041° W | 24.902° | 2025-09-14 19:34:48.050Z | 320.82° NNW |
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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