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LEMUR 2 LEIA-PHILIP, 63246

Orbit data source: Space-Track

LEMUR 2 LEIA-PHILIP, 63246 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
63246, 2025-052AN
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)
Icon of a cake. It is the launch day of the satellite!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, Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 LEMUR 2 LEIA-PHILIP
1 63246U 25052AN  26074.63221800  .00005553  00000-0  49091-3 0  9990
2 63246  97.6943 328.1303 0004018 161.0093 199.1279 14.96715067 54670
Epoch: 2026-03-15T15:10Z
TLE epoch observation values (Epoch: 2026-03-15T15:10:23.635Z)
Latitude
-0.00002°
Longitude
-72.70444°
Altitude
582.746 km
Speed
7.568 km/s
True Right ascension
21h 52m 31s
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
04:03:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.857 km
Perigee altitude
571.27 km
Semi-major axis
6,952.201 km
Eccentricity
0.0004
Inclination
97.6943°
RAAN
328.1303°
Arg. of periapsis
161.0093°
True anomaly
199.11282°
Mean anomaly
199.1279°
Eccentric anomaly
199.12036°
Mean motion
3.74421 °/min
Orbital period
96.15 mins
BSTAR
0.00049091
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Documentation

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