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, 0.5 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 LEMUR 2 STAR-FOX
1 62696U 25009CR 26262.49217043 .00004620 00000-0 34248-3 0 9999
2 62696 97.6885 343.4465 0003366 124.7226 235.4317 15.03586690 91722Epoch: 2026-09-19T11:48Z
TLE epoch observation values (Epoch: 2026-09-19T11:48:43.525Z)
Latitude
0.00002°
Longitude
167.86521°
Altitude
560.232 km
Speed
7.581 km/s
True Right ascension
22h 53m 47s
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
12:09:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
555.18 km
Perigee altitude
550.514 km
Semi-major axis
6,930.984 km
Eccentricity
0.00034
Inclination
97.6885°
RAAN
343.4465°
Arg. of periapsis
124.7226°
True anomaly
235.39995°
Mean anomaly
235.4317°
Eccentric anomaly
235.41582°
Mean motion
3.76141 °/min
Orbital period
95.71 mins
BSTAR
0.00034248
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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 | 2026-09-20 05:30:18.194Z | 165.293° S | 2026-09-20 05:33:18.194Z | 152.793° SSE | 77.487° | 2026-09-20 05:37:18.194Z | 348.554° N |
| 5 mins | 2026-09-20 18:44:18.194Z | 350.763° N | 2026-09-20 18:46:18.194Z | 291.924° WNW | 50.071° | 2026-09-20 18:49:18.194Z | 215.026° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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