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 26080.14546960 .00002235 00000-0 21103-3 0 9996
2 62694 97.7055 160.1716 0002561 356.7638 3.3566 14.94738944 64204Epoch: 2026-03-21T03:29Z
TLE epoch observation values (Epoch: 2026-03-21T03:29:28.573Z)
Latitude
0.00003°
Longitude
-70.86784°
Altitude
584.45 km
Speed
7.569 km/s
True Right ascension
10h 40m 41s
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
03:58:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
581.978 km
Perigee altitude
578.414 km
Semi-major axis
6,958.333 km
Eccentricity
0.00026
Inclination
97.7055°
RAAN
160.1716°
Arg. of periapsis
356.7638°
True anomaly
3.35832°
Mean anomaly
3.3566°
Eccentric anomaly
3.35746°
Mean motion
3.73926 °/min
Orbital period
96.28 mins
BSTAR
0.00021103
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-22 05:19:07.980Z | 168.576° S | 2026-03-22 05:22:07.980Z | 180.278° SSW | 43.226° | 2026-03-22 05:26:07.980Z | 346.385° N |
| 5 mins | 2026-03-22 18:38:07.980Z | 341.015° N | 2026-03-22 18:40:07.980Z | 281.867° WNW | 33.486° | 2026-03-22 18:43:07.980Z | 221.103° SW |
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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