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: 8 hours ago
TLE from 8 hours ago
0 LEMUR 2 WILSON
1 62694U 25009CP 26238.22487807 .00002241 00000-0 20792-3 0 9994
2 62694 97.6987 315.4564 0004085 143.5052 216.6448 14.95414247 87827Epoch: 2026-08-26T05:23Z
TLE epoch observation values (Epoch: 2026-08-26T05:23:49.465Z)
Latitude
-0.00001°
Longitude
-99.98064°
Altitude
586.418 km
Speed
7.566 km/s
True Right ascension
21h 01m 49s
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
04:39:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.94 km
Perigee altitude
575.257 km
Semi-major axis
6,956.236 km
Eccentricity
0.00041
Inclination
97.6987°
RAAN
315.4564°
Arg. of periapsis
143.5052°
True anomaly
216.61687°
Mean anomaly
216.6448°
Eccentric anomaly
216.63084°
Mean motion
3.74095 °/min
Orbital period
96.23 mins
BSTAR
0.00020792
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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 | 2026-08-26 17:13:15.134Z | 47.956° ENE | 2026-08-26 17:16:15.134Z | 98.406° ESE | 19.203° | 2026-08-26 17:18:15.134Z | 133.535° SE |
| 5 mins | 2026-08-26 18:49:15.134Z | 336.3° NNW | 2026-08-26 18:51:15.134Z | 293.88° NW | 25.865° | 2026-08-26 18:54:15.134Z | 234.974° WSW |
| 6 mins | 2026-08-27 05:37:15.134Z | 193.566° SSW | 2026-08-27 05:39:15.134Z | 237.927° WSW | 36.052° | 2026-08-27 05:43:15.134Z | 334.566° 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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