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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 LEMUR 2 STAR-FOX
1 62696U 25009CR 26170.75664247 .00006185 00000-0 46976-3 0 9997
2 62696 97.6953 252.3469 0004084 105.6897 254.4778 15.02534850 77940Epoch: 2026-06-19T18:09Z
TLE epoch observation values (Epoch: 2026-06-19T18:09:33.909Z)
Latitude
-0.00008°
Longitude
71.97458°
Altitude
562.901 km
Speed
7.579 km/s
True Right ascension
16h 49m 23s
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
07:18:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
558.917 km
Perigee altitude
553.253 km
Semi-major axis
6,934.222 km
Eccentricity
0.00041
Inclination
97.6953°
RAAN
252.3469°
Arg. of periapsis
105.6897°
True anomaly
254.43271°
Mean anomaly
254.4778°
Eccentric anomaly
254.45526°
Mean motion
3.75878 °/min
Orbital period
95.78 mins
BSTAR
0.00046976
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-21 05:26:53.223Z | 164.506° S | 2026-06-21 05:29:53.223Z | 134.272° SE | 44.66° | 2026-06-21 05:33:53.223Z | 348.929° N |
| 6 mins | 2026-06-21 18:40:53.223Z | 354.642° N | 2026-06-21 18:42:53.223Z | 312.967° NW | 36.338° | 2026-06-21 18:46:53.223Z | 211.604° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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