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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 LEMUR 2 LIA-MARTIN
1 63248U 25052AQ 26259.51187484 .00004431 00000-0 37588-3 0 9995
2 63248 97.6735 150.5075 0001660 204.3648 155.7496 14.98441287 82358Epoch: 2026-09-16T12:17Z
TLE epoch observation values (Epoch: 2026-09-16T12:17:05.986Z)
Latitude
-0.00005°
Longitude
-29.22984°
Altitude
575.817 km
Speed
7.572 km/s
True Right ascension
10h 02m 01s
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
02:59:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.871 km
Perigee altitude
567.565 km
Semi-major axis
6,946.855 km
Eccentricity
0.00017
Inclination
97.6735°
RAAN
150.5075°
Arg. of periapsis
204.3648°
True anomaly
155.75741°
Mean anomaly
155.7496°
Eccentric anomaly
155.75351°
Mean motion
3.74853 °/min
Orbital period
96.04 mins
BSTAR
0.00037588
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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 | 2026-09-17 17:15:53.110Z | 194.992° SSW | 2026-09-17 17:18:53.110Z | 280.48° WNW | 43.87° | 2026-09-17 17:21:53.110Z | 332.567° NNW |
| 5 mins | 2026-09-18 04:56:53.110Z | 56.92° ENE | 2026-09-18 04:58:53.110Z | 98.15° ESE | 23.956° | 2026-09-18 05:01:53.110Z | 148.543° SSE |
| 5 mins | 2026-09-18 06:31:53.110Z | 330.578° NNW | 2026-09-18 06:33:53.110Z | 289.459° WNW | 24.807° | 2026-09-18 06:36:53.110Z | 237.918° WSW |
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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