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: 19 hours ago
TLE from 19 hours ago
0 LEMUR 2 WILSON
1 62694U 25009CP 26171.17348258 .00001990 00000-0 18637-3 0 9995
2 62694 97.7027 249.5857 0004107 50.1741 309.9840 14.95177642 77802Epoch: 2026-06-20T04:09Z
TLE epoch observation values (Epoch: 2026-06-20T04:09:48.894Z)
Latitude
-0.00012°
Longitude
-81.25991°
Altitude
583.033 km
Speed
7.57 km/s
True Right ascension
16h 38m 20s
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
10:18:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
581.69 km
Perigee altitude
575.976 km
Semi-major axis
6,956.97 km
Eccentricity
0.00041
Inclination
97.7027°
RAAN
249.5857°
Arg. of periapsis
50.1741°
True anomaly
309.94793°
Mean anomaly
309.984°
Eccentric anomaly
309.96596°
Mean motion
3.74036 °/min
Orbital period
96.25 mins
BSTAR
0.00018637
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 04:24:33.604Z | 111.071° ESE | 2026-06-21 04:26:33.604Z | 76.278° E | 20.473° | 2026-06-21 04:29:33.604Z | 22.548° NE |
| 5 mins | 2026-06-21 06:00:33.604Z | 227.728° WSW | 2026-06-21 06:02:33.604Z | 275.411° WNW | 24.191° | 2026-06-21 06:05:33.604Z | 322.638° NNW |
| 6 mins | 2026-06-21 17:41:33.604Z | 38.555° NE | 2026-06-21 17:43:33.604Z | 84.83° E | 33.005° | 2026-06-21 17:47:33.604Z | 168.941° S |
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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