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LEMUR 2 LIA-MARTIN, 63248

Orbit data source: Space-Track

LEMUR 2 LIA-MARTIN, 63248 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
63248, 2025-052AQ
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, Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago
0 LEMUR 2 LIA-MARTIN
1 63248U 25052AQ  26120.70230786  .00005150  00000-0  44812-3 0  9994
2 63248  97.6941  13.8596 0003160  18.4780 341.6556 14.97369495 61577
Epoch: 2026-04-30T16:51Z
TLE epoch observation values (Epoch: 2026-04-30T16:51:19.399Z)
Latitude
-0.00002°
Longitude
-97.61635°
Altitude
575.993 km
Speed
7.574 km/s
True Right ascension
00h 55m 26s
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
20:33:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.233 km
Perigee altitude
569.84 km
Semi-major axis
6,950.173 km
Eccentricity
0.00032
Inclination
97.6941°
RAAN
13.8596°
Arg. of periapsis
18.478°
True anomaly
341.6442°
Mean anomaly
341.6556°
Eccentric anomaly
341.6499°
Mean motion
3.74584 °/min
Orbital period
96.11 mins
BSTAR
0.00044812
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