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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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: 21 hours ago
TLE from 21 hours ago
0 LEMUR 2 WILSON
1 62694U 25009CP 26067.76083588 .00004620 00000-0 43119-3 0 9992
2 62694 97.7069 148.0059 0003602 39.4240 320.7242 14.94673795 62358Epoch: 2026-03-08T18:15Z
TLE epoch observation values (Epoch: 2026-03-08T18:15:36.220Z)
Latitude
-0°
Longitude
67.64148°
Altitude
584.491 km
Speed
7.569 km/s
True Right ascension
09h 52m 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
19:18:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.905 km
Perigee altitude
577.892 km
Semi-major axis
6,958.535 km
Eccentricity
0.00036
Inclination
97.7069°
RAAN
148.0059°
Arg. of periapsis
39.424°
True anomaly
320.69806°
Mean anomaly
320.7242°
Eccentric anomaly
320.71113°
Mean motion
3.73909 °/min
Orbital period
96.28 mins
BSTAR
0.00043119
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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 | 2026-03-09 17:19:47.227Z | 42.491° NE | 2026-03-09 17:22:47.227Z | 90.892° ESE | 21.429° | 2026-03-09 17:25:47.227Z | 144.13° SSE |
| 4 mins | 2026-03-09 18:56:47.227Z | 324.265° NNW | 2026-03-09 18:58:47.227Z | 278.129° WNW | 23.328° | 2026-03-09 19:00:47.227Z | 242.446° WSW |
| 6 mins | 2026-03-10 05:44:47.227Z | 202.257° SSW | 2026-03-10 05:46:47.227Z | 254.371° W | 33.938° | 2026-03-10 05:50:47.227Z | 333.202° 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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