LEMUR 2 STAR-FOX, 62696
Orbit data source: Space-Track
LEMUR 2 STAR-FOX, 62696 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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62696 intel report (Beta)
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Edit Public Description
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, 0.2 m
Radar Cross Section
0.063 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 LEMUR 2 STAR-FOX
1 62696U 25009CR 25286.17493372 .00017988 00000-0 15531-2 0 9994
2 62696 97.7290 4.9638 0003766 108.5785 251.5846 14.97295607 40523Epoch: 2025-10-13T04:11Z
TLE epoch observation values (Epoch: 2025-10-13T04:11:54.273Z)
Latitude
-0.00004°
Longitude
-79.99382°
Altitude
579.135 km
Speed
7.571 km/s
True Right ascension
00h 19m 51s
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
08:59:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.884 km
Perigee altitude
569.649 km
Semi-major axis
6,950.404 km
Eccentricity
0.00038
Inclination
97.729°
RAAN
4.9638°
Arg. of periapsis
108.5785°
True anomaly
251.54366°
Mean anomaly
251.5846°
Eccentric anomaly
251.56413°
Mean motion
3.74566 °/min
Orbital period
96.11 mins
BSTAR
0.0015531
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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 STAR-FOX 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 | 2025-10-13 17:35:58.044Z | 35.779° NE | 2025-10-13 17:38:58.044Z | 84.694° E | 25.969° | 2025-10-13 17:41:58.044Z | 150.09° SSE |
| 4 mins | 2025-10-13 19:12:58.044Z | 320.006° NNW | 2025-10-13 19:13:58.044Z | 301.364° NW | 18.713° | 2025-10-13 19:16:58.044Z | 248.934° W |
| 5 mins | 2025-10-14 05:59:58.044Z | 213.027° SW | 2025-10-14 06:01:58.044Z | 260.118° W | 28.321° | 2025-10-14 06:04:58.044Z | 321.809° 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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