LEMUR 2 JIN-LUEN, 43182
Orbit data source: Space-Track
LEMUR 2 JIN-LUEN, 43182 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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43182 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 JIN-LUEN
1 43182U 18014C 25256.73639110 .00034911 00000-0 81446-3 0 9996
2 43182 97.5481 171.8717 0007157 168.7597 191.3811 15.42122828417943Epoch: 2025-09-13T17:40Z
TLE epoch observation values (Epoch: 2025-09-13T17:40:24.191Z)
Latitude
0.00002°
Longitude
-86.19457°
Altitude
447.746 km
Speed
7.641 km/s
True Right ascension
11h 27m 29s
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
00:46:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.665 km
Perigee altitude
431.91 km
Semi-major axis
6,814.925 km
Eccentricity
0.00072
Inclination
97.5481°
RAAN
171.8717°
Arg. of periapsis
168.7597°
True anomaly
191.36493°
Mean anomaly
191.3811°
Eccentric anomaly
191.37301°
Mean motion
3.85791 °/min
Orbital period
93.31 mins
BSTAR
0.00081446
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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 JIN-LUEN 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-14 18:43:46.039Z | 189.934° SSW | 2025-09-14 18:45:46.039Z | 266.147° W | 38.367° | 2025-09-14 18:48:46.039Z | 337.209° NNW |
| 5 mins | 2025-09-15 07:36:46.039Z | 353.697° N | 2025-09-15 07:38:46.039Z | 291.832° WNW | 36.58° | 2025-09-15 07:41:46.039Z | 211.389° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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