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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 LEMUR 2 LIA-MARTIN
1 63248U 25052AQ 26074.51924147 .00006400 00000-0 56247-3 0 9996
2 63248 97.7010 328.3876 0004598 121.4082 238.7590 14.96889246 54662Epoch: 2026-03-15T12:27Z
TLE epoch observation values (Epoch: 2026-03-15T12:27:42.463Z)
Latitude
0.00002°
Longitude
-31.66424°
Altitude
581.225 km
Speed
7.569 km/s
True Right ascension
21h 53m 33s
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
04:02:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
576.721 km
Perigee altitude
570.328 km
Semi-major axis
6,951.661 km
Eccentricity
0.00046
Inclination
97.701°
RAAN
328.3876°
Arg. of periapsis
121.4082°
True anomaly
238.71396°
Mean anomaly
238.759°
Eccentric anomaly
238.73648°
Mean motion
3.74464 °/min
Orbital period
96.14 mins
BSTAR
0.00056247
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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 | 2026-03-16 05:04:34.310Z | 36.421° NE | 2026-03-16 05:07:34.310Z | 86.344° E | 25.854° | 2026-03-16 05:10:34.310Z | 150.28° SSE |
| 4 mins | 2026-03-16 06:41:34.310Z | 319.69° NNW | 2026-03-16 06:42:34.310Z | 300.85° NW | 18.926° | 2026-03-16 06:45:34.310Z | 248.361° W |
| 4 mins | 2026-03-16 15:54:34.310Z | 90.217° ESE | 2026-03-16 15:55:34.310Z | 71.828° E | 17.533° | 2026-03-16 15:58:34.310Z | 23.654° NE |
| 5 mins | 2026-03-16 17:28:34.310Z | 210.589° SW | 2026-03-16 17:30:34.310Z | 255.081° W | 28.47° | 2026-03-16 17:33:34.310Z | 320.623° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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