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, 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 MARACHE-FRAN
1 63262U 25052BE 26171.20365968 .00004017 00000-0 32663-3 0 9994
2 63262 97.6933 64.7998 0005047 11.9319 348.2023 15.00125665 69212Epoch: 2026-06-20T04:53Z
TLE epoch observation values (Epoch: 2026-06-20T04:53:16.196Z)
Latitude
-0.00003°
Longitude
83.06067°
Altitude
566.132 km
Speed
7.58 km/s
True Right ascension
04h 19m 11s
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
07:21:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
567.017 km
Perigee altitude
560.01 km
Semi-major axis
6,941.65 km
Eccentricity
0.0005
Inclination
97.6933°
RAAN
64.7998°
Arg. of periapsis
11.9319°
True anomaly
348.19047°
Mean anomaly
348.2023°
Eccentric anomaly
348.19638°
Mean motion
3.75275 °/min
Orbital period
95.93 mins
BSTAR
0.00032663
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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 | 2026-06-21 05:28:26.211Z | 27.709° NE | 2026-06-21 05:31:26.211Z | 98.345° ESE | 37.318° | 2026-06-21 05:34:26.211Z | 171.308° S |
| 5 mins | 2026-06-21 16:15:26.211Z | 118.084° SE | 2026-06-21 16:17:26.211Z | 78.322° E | 24.62° | 2026-06-21 16:20:26.211Z | 17.804° NNE |
| 4 mins | 2026-06-21 17:51:26.211Z | 238.589° WSW | 2026-06-21 17:52:26.211Z | 258.338° W | 19.307° | 2026-06-21 17:55:26.211Z | 311.289° NW |
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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