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: 16 hours ago
TLE from 16 hours ago
0 LEMUR 2 LIA-MARTIN
1 63248U 25052AQ 26212.69609247 .00004476 00000-0 38248-3 0 9992
2 63248 97.6815 104.4341 0003994 54.9205 305.2392 14.98142906 75345Epoch: 2026-07-31T16:42Z
TLE epoch observation values (Epoch: 2026-07-31T16:42:22.389Z)
Latitude
0.00003°
Longitude
-95.47775°
Altitude
574.086 km
Speed
7.575 km/s
True Right ascension
06h 57m 44s
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
22:00:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.416 km
Perigee altitude
566.867 km
Semi-major axis
6,947.778 km
Eccentricity
0.0004
Inclination
97.6815°
RAAN
104.4341°
Arg. of periapsis
54.9205°
True anomaly
305.20181°
Mean anomaly
305.2392°
Eccentric anomaly
305.22051°
Mean motion
3.74778 °/min
Orbital period
96.06 mins
BSTAR
0.00038248
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-01 16:52:36.405Z | 167.385° S | 2026-08-01 16:55:36.405Z | 178.513° S | 44.701° | 2026-08-01 16:59:36.405Z | 347.374° N |
| 6 mins | 2026-08-02 06:08:36.405Z | 353.103° N | 2026-08-02 06:11:36.405Z | 277.558° WNW | 34.837° | 2026-08-02 06:14:36.405Z | 217.867° SW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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