Showing default

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.

Loading next visibility...
Identifier
62696, 2025-009CR
Orbit
SSO
Country
Flag of USUS
Related 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)
2025-01-14 (11 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.063 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 LEMUR 2 STAR-FOX
1 62696U 25009CR  25339.94383181  .00013587  00000-0  11298-2 0  9991
2 62696  97.7242  58.1889 0002184 280.4384  79.6592 14.98824813 48575
Epoch: 2025-12-05T22:39Z
TLE epoch observation values (Epoch: 2025-12-05T22:39:07.068Z)
Latitude
-0.00007°
Longitude
3.43079°
Altitude
573.306 km
Speed
7.574 km/s
True Right ascension
03h 52m 45s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:44:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.051 km
Perigee altitude
566.017 km
Semi-major axis
6,945.671 km
Eccentricity
0.00022
Inclination
97.7242°
RAAN
58.1889°
Arg. of periapsis
280.4384°
True anomaly
79.68382°
Mean anomaly
79.6592°
Eccentric anomaly
79.67151°
Mean motion
3.74949 °/min
Orbital period
96.01 mins
BSTAR
0.0011298
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|