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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 LEMUR 2 STAR-FOX
1 62696U 25009CR 26124.99431066 .00007112 00000-0 54898-3 0 9996
2 62696 97.6892 206.9573 0000315 146.3746 213.7499 15.01865251 71078Epoch: 2026-05-04T23:51Z
TLE epoch observation values (Epoch: 2026-05-04T23:51:48.441Z)
Latitude
0.00006°
Longitude
-13.87007°
Altitude
564.384 km
Speed
7.579 km/s
True Right ascension
13h 47m 49s
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
16:45:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
558.366 km
Perigee altitude
557.929 km
Semi-major axis
6,936.284 km
Eccentricity
0.00003
Inclination
97.6892°
RAAN
206.9573°
Arg. of periapsis
146.3746°
True anomaly
213.74789°
Mean anomaly
213.7499°
Eccentric anomaly
213.7489°
Mean motion
3.7571 °/min
Orbital period
95.82 mins
BSTAR
0.00054898
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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 | 2026-05-05 18:01:28.055Z | 25.935° NE | 2026-05-05 18:04:28.055Z | 96.776° ESE | 38.504° | 2026-05-05 18:07:28.055Z | 173.487° S |
| 4 mins | 2026-05-06 04:48:28.055Z | 108.438° ESE | 2026-05-06 04:50:28.055Z | 58.302° ENE | 25.016° | 2026-05-06 04:52:28.055Z | 20.034° NNE |
| 4 mins | 2026-05-06 06:23:28.055Z | 236.365° WSW | 2026-05-06 06:25:28.055Z | 275.967° WNW | 18.443° | 2026-05-06 06:27:28.055Z | 308.72° NW |
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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