LEMUR 2 LEIA-PHILIP, 63246
Orbit data source: Space-Track
LEMUR 2 LEIA-PHILIP, 63246 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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63246 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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 LEMUR 2 LEIA-PHILIP
1 63246U 25052AN 26219.65848581 .00001126 00000-0 10169-3 0 9990
2 63246 97.6769 110.7282 0005722 66.5768 293.6056 14.97447041 76377Epoch: 2026-08-07T15:48Z
TLE epoch observation values (Epoch: 2026-08-07T15:48:13.173Z)
Latitude
0.00002°
Longitude
-82.50771°
Altitude
576.248 km
Speed
7.573 km/s
True Right ascension
07h 22m 54s
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
21:08:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.772 km
Perigee altitude
567.819 km
Semi-major axis
6,949.932 km
Eccentricity
0.00057
Inclination
97.6769°
RAAN
110.7282°
Arg. of periapsis
66.5768°
True anomaly
293.5455°
Mean anomaly
293.6056°
Eccentric anomaly
293.57555°
Mean motion
3.74604 °/min
Orbital period
96.1 mins
BSTAR
0.00010169
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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 LEIA-PHILIP 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 | 2026-08-08 16:00:02.720Z | 120.126° SE | 2026-08-08 16:03:02.720Z | 69.258° E | 21.584° | 2026-08-08 16:06:02.720Z | 18.148° NNE |
| 5 mins | 2026-08-08 17:36:02.720Z | 221.02° SW | 2026-08-08 17:38:02.720Z | 261.364° W | 23.083° | 2026-08-08 17:41:02.720Z | 316.601° NNW |
| 6 mins | 2026-08-09 05:16:02.720Z | 32.716° NE | 2026-08-09 05:19:02.720Z | 106.749° ESE | 34.136° | 2026-08-09 05:22:02.720Z | 167.512° 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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