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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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: 1 day ago
TLE from 1 day ago
0 LEMUR 2 MARACHE-FRAN
1 63262U 25052BE 26083.66132405 .00006545 00000-0 54300-3 0 9994
2 63262 97.7002 338.3038 0002056 33.1086 327.0266 14.99126862 56092Epoch: 2026-03-24T15:52Z
TLE epoch observation values (Epoch: 2026-03-24T15:52:18.397Z)
Latitude
0.00002°
Longitude
-81.90863°
Altitude
571.448 km
Speed
7.576 km/s
True Right ascension
22h 33m 12s
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
20:37:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.027 km
Perigee altitude
565.171 km
Semi-major axis
6,944.736 km
Eccentricity
0.00021
Inclination
97.7002°
RAAN
338.3038°
Arg. of periapsis
33.1086°
True anomaly
327.01377°
Mean anomaly
327.0266°
Eccentric anomaly
327.02019°
Mean motion
3.75024 °/min
Orbital period
95.99 mins
BSTAR
0.000543
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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 | 2026-03-25 16:03:11.533Z | 110.852° ESE | 2026-03-25 16:05:11.533Z | 76.926° E | 19.559° | 2026-03-25 16:08:11.533Z | 23.445° NE |
| 5 mins | 2026-03-25 17:38:11.533Z | 214.684° SW | 2026-03-25 17:40:11.533Z | 254.277° W | 24.799° | 2026-03-25 17:43:11.533Z | 316.226° NNW |
| 6 mins | 2026-03-26 05:18:11.533Z | 41.48° NE | 2026-03-26 05:20:11.533Z | 87.388° E | 30.849° | 2026-03-26 05:24:11.533Z | 166.475° S |
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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