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LEMUR 2 THEFALCONER, 63264

Orbit data source: Space-Track

LEMUR 2 THEFALCONER, 63264 is a payload satellite owned by Spire (US) in SSO that was launched on Sat, 15 Mar 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
63264, 2025-052BG
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Spire/Glasgow
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
2025-03-15 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 LEMUR 2 THEFALCONER
1 63264U 25052BG  26166.60737772  .00002511  00000-0  22108-3 0  9990
2 63264  97.6873  59.0093 0002871  38.0678 322.0746 14.97381879 68453
Epoch: 2026-06-15T14:34Z
TLE epoch observation values (Epoch: 2026-06-15T14:34:37.435Z)
Latitude
-0.00004°
Longitude
-63.53801°
Altitude
576.466 km
Speed
7.573 km/s
True Right ascension
03h 56m 02s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
13:38:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.993 km
Perigee altitude
570.002 km
Semi-major axis
6,950.135 km
Eccentricity
0.00029
Inclination
97.6873°
RAAN
59.0093°
Arg. of periapsis
38.0678°
True anomaly
322.05437°
Mean anomaly
322.0746°
Eccentric anomaly
322.06449°
Mean motion
3.74588 °/min
Orbital period
96.11 mins
BSTAR
0.00022108
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