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, 0.5 m
Radar Cross Section
0.124 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 LEMUR 2 JIN-LUEN
1 43182U 18014C 25295.48068226 .00062689 00000-0 12280-2 0 9997
2 43182 97.5484 212.1035 0009789 69.8925 290.3377 15.47124604423928Epoch: 2025-10-22T11:32Z
TLE epoch observation values (Epoch: 2025-10-22T11:32:10.947Z)
Latitude
0°
Longitude
7.90421°
Altitude
425.956 km
Speed
7.657 km/s
True Right ascension
14h 08m 24s
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
17:54:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
428.735 km
Perigee altitude
415.422 km
Semi-major axis
6,800.215 km
Eccentricity
0.00098
Inclination
97.5484°
RAAN
212.1035°
Arg. of periapsis
69.8925°
True anomaly
290.23247°
Mean anomaly
290.3377°
Eccentric anomaly
290.28509°
Mean motion
3.87043 °/min
Orbital period
93.01 mins
BSTAR
0.001228
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-23 06:43:49.657Z | 47.417° ENE | 2025-10-23 06:45:49.657Z | 86.396° E | 18.326° | 2025-10-23 06:47:49.657Z | 133.8° SE |
| 4 mins | 2025-10-23 18:43:49.657Z | 180.505° SSW | 2025-10-23 18:44:49.657Z | 210.912° SW | 42.09° | 2025-10-23 18:47:49.657Z | 342.697° N |
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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