Showing default

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.

Loading next visibility...
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 (9 months 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: 22 hours ago

TLE from 22 hours ago
0 LEMUR 2 THEFALCONER
1 63264U 25052BG  25334.21694334  .00007089  00000-0  65057-3 0  9994
2 63264  97.7057 224.8480 0001826 353.3092   6.8104 14.95156997 38936
Epoch: 2025-11-30T05:12Z
TLE epoch observation values (Epoch: 2025-11-30T05:12:23.904Z)
Latitude
-0.00004°
Longitude
77.41443°
Altitude
583.671 km
Speed
7.569 km/s
True Right ascension
14h 59m 23s
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
01:16:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.168 km
Perigee altitude
577.627 km
Semi-major axis
6,957.034 km
Eccentricity
0.00018
Inclination
97.7057°
RAAN
224.848°
Arg. of periapsis
353.3092°
True anomaly
6.81288°
Mean anomaly
6.8104°
Eccentric anomaly
6.81164°
Mean motion
3.7403 °/min
Orbital period
96.25 mins
BSTAR
0.00065057
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
|