LEMUR 2 WILSON, 62694
Orbit data source: Space-Track
LEMUR 2 WILSON, 62694 is a payload satellite owned by Spire (US) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62694 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
7.6 kg wet, 7.6 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 LEMUR 2 WILSON
1 62694U 25009CP 25286.22917966 .00005640 00000-0 54122-3 0 9990
2 62694 97.7250 4.0056 0004610 129.5805 230.5823 14.93474777 40476Epoch: 2025-10-13T05:30Z
TLE epoch observation values (Epoch: 2025-10-13T05:30:01.122Z)
Latitude
0.00001°
Longitude
-100.53404°
Altitude
592.196 km
Speed
7.563 km/s
True Right ascension
00h 16m 01s
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
08:59:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.336 km
Perigee altitude
580.916 km
Semi-major axis
6,962.263 km
Eccentricity
0.00046
Inclination
97.725°
RAAN
4.0056°
Arg. of periapsis
129.5805°
True anomaly
230.5415°
Mean anomaly
230.5823°
Eccentric anomaly
230.5619°
Mean motion
3.73609 °/min
Orbital period
96.36 mins
BSTAR
0.00054122
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Other satellites on launch #9 in the year 2025 (2025-01-14 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 WILSON 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-13 17:19:58.543Z | 43.151° NE | 2025-10-13 17:22:58.543Z | 90.819° ESE | 20.708° | 2025-10-13 17:25:58.543Z | 143.021° SSE |
| 5 mins | 2025-10-13 18:56:58.543Z | 326.551° NNW | 2025-10-13 18:58:58.543Z | 279.886° WNW | 24.207° | 2025-10-13 19:01:58.543Z | 232.745° WSW |
| 6 mins | 2025-10-14 05:44:58.543Z | 195.308° SSW | 2025-10-14 05:47:58.543Z | 271.593° WNW | 34.456° | 2025-10-14 05:50:58.543Z | 330.266° 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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