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: 11 hours ago
TLE from 11 hours ago
0 LEMUR 2 MARACHE-FRAN
1 63262U 25052BE 26074.65004874 .00007051 00000-0 58656-3 0 9992
2 63262 97.7000 329.4013 0002400 44.7141 315.4275 14.98997805 54740Epoch: 2026-03-15T15:36Z
TLE epoch observation values (Epoch: 2026-03-15T15:36:04.211Z)
Latitude
-0.00001°
Longitude
-77.87008°
Altitude
571.857 km
Speed
7.576 km/s
True Right ascension
21h 57m 36s
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
07:23:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.665 km
Perigee altitude
565.331 km
Semi-major axis
6,945.135 km
Eccentricity
0.00024
Inclination
97.7°
RAAN
329.4013°
Arg. of periapsis
44.7141°
True anomaly
315.40819°
Mean anomaly
315.4275°
Eccentric anomaly
315.41785°
Mean motion
3.74992 °/min
Orbital period
96 mins
BSTAR
0.00058656
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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 | 2026-03-16 05:00:01.037Z | 46.921° ENE | 2026-03-16 05:03:01.037Z | 102.866° ESE | 21.479° | 2026-03-16 05:05:01.037Z | 139.478° SSE |
| 5 mins | 2026-03-16 06:36:01.037Z | 327.415° NNW | 2026-03-16 06:38:01.037Z | 283.575° WNW | 22.762° | 2026-03-16 06:41:01.037Z | 235.386° WSW |
| 6 mins | 2026-03-16 17:22:01.037Z | 197.371° SSW | 2026-03-16 17:25:01.037Z | 281.772° WNW | 33.234° | 2026-03-16 17:28:01.037Z | 331.844° 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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