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: 20 hours ago
TLE from 20 hours ago
0 LEMUR 2 WILSON
1 62694U 25009CP 26287.47005452 .00001663 00000-0 15500-3 0 9995
2 62694 97.6933 3.8126 0003274 22.8109 337.3257 14.95568302 95180Epoch: 2026-10-14T11:16Z
TLE epoch observation values (Epoch: 2026-10-14T11:16:52.710Z)
Latitude
-0.00002°
Longitude
171.57366°
Altitude
581.556 km
Speed
7.571 km/s
True Right ascension
00h 15m 15s
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
02:17:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.898 km
Perigee altitude
575.343 km
Semi-major axis
6,955.757 km
Eccentricity
0.00033
Inclination
97.6933°
RAAN
3.8126°
Arg. of periapsis
22.8109°
True anomaly
337.31123°
Mean anomaly
337.3257°
Eccentric anomaly
337.31847°
Mean motion
3.74133 °/min
Orbital period
96.22 mins
BSTAR
0.000155
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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 | 2026-10-15 18:21:45.360Z | 0.03° NNE | 2026-10-15 18:24:45.360Z | 272.116° WNW | 58.37° | 2026-10-15 18:27:45.360Z | 208.96° SW |
| 6 mins | 2026-10-16 05:09:45.360Z | 160.742° S | 2026-10-16 05:12:45.360Z | 48.82° ENE | 77.041° | 2026-10-16 05:15:45.360Z | 351.48° N |
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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