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: 9 hours ago
TLE from 9 hours ago
0 LEMUR 2 LIA-MARTIN
1 63248U 25052AQ 26027.64961623 .00010504 00000-0 93510-3 0 9992
2 63248 97.7063 282.2394 0002088 336.6923 23.4204 14.96231599 47653Epoch: 2026-01-27T15:35Z
TLE epoch observation values (Epoch: 2026-01-27T15:35:26.842Z)
Latitude
0.00006°
Longitude
-78.55043°
Altitude
580.269 km
Speed
7.571 km/s
True Right ascension
18h 48m 57s
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
01:45:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.015 km
Perigee altitude
574.111 km
Semi-major axis
6,953.7 km
Eccentricity
0.00021
Inclination
97.7063°
RAAN
282.2394°
Arg. of periapsis
336.6923°
True anomaly
23.42991°
Mean anomaly
23.4204°
Eccentric anomaly
23.42516°
Mean motion
3.74299 °/min
Orbital period
96.18 mins
BSTAR
0.0009351
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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 | 2026-01-28 05:00:12.271Z | 38.691° NE | 2026-01-28 05:03:12.271Z | 87.017° E | 23.744° | 2026-01-28 05:06:12.271Z | 146.58° SSE |
| 4 mins | 2026-01-28 06:37:12.271Z | 322.334° NNW | 2026-01-28 06:39:12.271Z | 280.136° WNW | 20.86° | 2026-01-28 06:41:12.271Z | 246.314° WSW |
| 4 mins | 2026-01-28 15:50:12.271Z | 92.883° ESE | 2026-01-28 15:52:12.271Z | 58.111° ENE | 15.878° | 2026-01-28 15:54:12.271Z | 28.13° NE |
| 6 mins | 2026-01-28 17:24:12.271Z | 203.077° SW | 2026-01-28 17:27:12.271Z | 278.929° WNW | 30.356° | 2026-01-28 17:30:12.271Z | 328.683° 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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