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LEMUR 2 ARIANNA, 62699

Orbit data source: Space-Track

LEMUR 2 ARIANNA, 62699 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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Identifier
62699, 2025-009CU
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 (2 years 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, Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 LEMUR 2 ARIANNA
1 62699U 25009CU  26215.76543527  .00007394  00000-0  55204-3 0  9995
2 62699  97.6866 296.7730 0000967 359.6854   0.4371 15.03122031 84704
Epoch: 2026-08-03T18:22Z
TLE epoch observation values (Epoch: 2026-08-03T18:22:13.607Z)
Latitude
0.00005°
Longitude
68.87245°
Altitude
559.665 km
Speed
7.582 km/s
True Right ascension
19h 47m 05s
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
21:32:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
554.947 km
Perigee altitude
553.606 km
Semi-major axis
6,932.414 km
Eccentricity
0.0001
Inclination
97.6866°
RAAN
296.773°
Arg. of periapsis
359.6854°
True anomaly
0.43718°
Mean anomaly
0.4371°
Eccentric anomaly
0.43714°
Mean motion
3.76025 °/min
Orbital period
95.74 mins
BSTAR
0.00055204
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