LEMUR 2 MARACHE-FRAN, 63262
Orbit data source: Space-Track
LEMUR 2 MARACHE-FRAN, 63262 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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63262 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, 14.5 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 MARACHE-FRAN
1 63262U 25052BE 25286.97599057 .00010059 00000-0 90231-3 0 9990
2 63262 97.7102 178.7638 0003801 106.4787 253.6852 14.95944433 31890Epoch: 2025-10-13T23:25Z
TLE epoch observation values (Epoch: 2025-10-13T23:25:25.585Z)
Latitude
-0.00002°
Longitude
164.63615°
Altitude
583.236 km
Speed
7.568 km/s
True Right ascension
11h 55m 03s
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
11:59:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.097 km
Perigee altitude
573.811 km
Semi-major axis
6,954.591 km
Eccentricity
0.00038
Inclination
97.7102°
RAAN
178.7638°
Arg. of periapsis
106.4787°
True anomaly
253.6434°
Mean anomaly
253.6852°
Eccentric anomaly
253.6643°
Mean motion
3.74228 °/min
Orbital period
96.2 mins
BSTAR
0.00090231
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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 MARACHE-FRAN 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-15 04:54:08.008Z | 48.105° ENE | 2025-10-15 04:57:08.008Z | 99.419° ESE | 19.465° | 2025-10-15 04:59:08.008Z | 134.56° SE |
| 5 mins | 2025-10-15 06:30:08.008Z | 334.829° NNW | 2025-10-15 06:32:08.008Z | 291.594° WNW | 25.535° | 2025-10-15 06:35:08.008Z | 234.737° WSW |
| 6 mins | 2025-10-15 17:18:08.008Z | 197.28° SSW | 2025-10-15 17:20:08.008Z | 253.724° W | 36.603° | 2025-10-15 17:24:08.008Z | 335.66° 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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