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: 17 hours ago
TLE from 17 hours ago
0 LEMUR 2 JIN-LUEN
1 43182U 18014C 25339.30367464 .00098400 00000-0 15087-2 0 9991
2 43182 97.5507 258.0222 0002307 245.9383 114.1629 15.53971587430710Epoch: 2025-12-05T07:17Z
TLE epoch observation values (Epoch: 2025-12-05T07:17:17.488Z)
Latitude
-0.00003°
Longitude
74.35164°
Altitude
408.917 km
Speed
7.665 km/s
True Right ascension
17h 12m 05s
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
22:41:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
403.635 km
Perigee altitude
400.507 km
Semi-major axis
6,780.208 km
Eccentricity
0.00023
Inclination
97.5507°
RAAN
258.0222°
Arg. of periapsis
245.9383°
True anomaly
114.18702°
Mean anomaly
114.1629°
Eccentric anomaly
114.17496°
Mean motion
3.88757 °/min
Orbital period
92.6 mins
BSTAR
0.0015087
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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 | 2025-12-06 07:01:51.948Z | 41.652° NE | 2025-12-06 07:03:51.948Z | 81.178° E | 20.921° | 2025-12-06 07:06:51.948Z | 152.159° SSE |
| 4 mins | 2025-12-06 18:58:51.948Z | 190.517° SSW | 2025-12-06 18:59:51.948Z | 236.528° WSW | 40.659° | 2025-12-06 19:02:51.948Z | 339.838° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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