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: 2 days ago
TLE from 2 days ago
0 LEMUR 2 STAR-FOX
1 62696U 25009CR 26215.76709363 .00008131 00000-0 60672-3 0 9999
2 62696 97.6926 297.0370 0000624 340.0302 20.0898 15.03109984 84708Epoch: 2026-08-03T18:24Z
TLE epoch observation values (Epoch: 2026-08-03T18:24:36.889Z)
Latitude
-0.00009°
Longitude
68.53783°
Altitude
559.966 km
Speed
7.582 km/s
True Right ascension
19h 48m 08s
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
21:32:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
554.747 km
Perigee altitude
553.882 km
Semi-major axis
6,932.451 km
Eccentricity
0.00006
Inclination
97.6926°
RAAN
297.037°
Arg. of periapsis
340.0302°
True anomaly
20.09226°
Mean anomaly
20.0898°
Eccentric anomaly
20.09103°
Mean motion
3.76022 °/min
Orbital period
95.74 mins
BSTAR
0.00060672
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-05 17:19:58.834Z | 57.972° ENE | 2026-08-05 17:21:58.834Z | 89.667° E | 15.082° | 2026-08-05 17:23:58.834Z | 123.161° SE |
| 5 mins | 2026-08-05 18:54:58.834Z | 341.883° N | 2026-08-05 18:56:58.834Z | 293.813° NW | 30.212° | 2026-08-05 18:59:58.834Z | 227.076° WSW |
| 6 mins | 2026-08-06 05:39:58.834Z | 179.842° S | 2026-08-06 05:41:58.834Z | 248.997° W | 43.243° | 2026-08-06 05:45:58.834Z | 343.028° 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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