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 25334.24941867 .00010290 00000-0 89784-3 0 9992
2 63262 97.7084 225.3473 0002437 24.9602 335.1737 14.97023683 38969Epoch: 2025-11-30T05:59Z
TLE epoch observation values (Epoch: 2025-11-30T05:59:09.773Z)
Latitude
-0.00002°
Longitude
66.1906°
Altitude
577.61 km
Speed
7.573 km/s
True Right ascension
15h 01m 23s
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
21:18:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.802 km
Perigee altitude
571.414 km
Semi-major axis
6,951.245 km
Eccentricity
0.00024
Inclination
97.7084°
RAAN
225.3473°
Arg. of periapsis
24.9602°
True anomaly
335.16197°
Mean anomaly
335.1737°
Eccentric anomaly
335.16784°
Mean motion
3.74498 °/min
Orbital period
96.13 mins
BSTAR
0.00089784
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-01 05:01:36.591Z | 45.394° ENE | 2025-12-01 05:04:36.591Z | 102.339° ESE | 22.825° | 2025-12-01 05:07:36.591Z | 151.166° SSE |
| 5 mins | 2025-12-01 06:37:36.591Z | 328.664° NNW | 2025-12-01 06:39:36.591Z | 287.689° WNW | 22.011° | 2025-12-01 06:42:36.591Z | 238.363° WSW |
| 6 mins | 2025-12-01 17:24:36.591Z | 200.788° SSW | 2025-12-01 17:27:36.591Z | 279.895° WNW | 31.534° | 2025-12-01 17:30:36.591Z | 329.938° 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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