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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63248 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated 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)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 LEMUR 2 LIA-MARTIN
1 63248U 25052AQ 25334.24714083 .00008569 00000-0 78403-3 0 9996
2 63248 97.7089 224.7696 0004615 115.0331 245.1370 14.95208081 38923Epoch: 2025-11-30T05:55Z
TLE epoch observation values (Epoch: 2025-11-30T05:55:52.967Z)
Latitude
0.00003°
Longitude
66.43516°
Altitude
586.127 km
Speed
7.566 km/s
True Right ascension
14h 59m 04s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:17:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
581.95 km
Perigee altitude
575.528 km
Semi-major axis
6,956.876 km
Eccentricity
0.00046
Inclination
97.7089°
RAAN
224.7696°
Arg. of periapsis
115.0331°
True anomaly
245.08903°
Mean anomaly
245.137°
Eccentric anomaly
245.11301°
Mean motion
3.74043 °/min
Orbital period
96.25 mins
BSTAR
0.00078403
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Other satellites on launch #52 in the year 2025 (2025-03-15 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.LEMUR 2 LIA-MARTIN Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-01 05:00:05.930Z | 46.176° ENE | 2025-12-01 05:03:05.930Z | 105.036° ESE | 23.095° | 2025-12-01 05:06:05.930Z | 152.532° SSE |
| 5 mins | 2025-12-01 06:36:05.930Z | 328.431° NNW | 2025-12-01 06:38:05.930Z | 287.987° WNW | 21.718° | 2025-12-01 06:41:05.930Z | 238.98° WSW |
| 6 mins | 2025-12-01 17:24:05.930Z | 204.524° SW | 2025-12-01 17:26:05.930Z | 249.469° W | 31.211° | 2025-12-01 17:30:05.930Z | 330.193° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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