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: 6 hours ago
TLE from 6 hours ago
0 LEMUR 2 LEIA-PHILIP
1 63246U 25052AN 26220.59399047 .00000868 00000-0 79558-4 0 9993
2 63246 97.6768 111.6475 0005675 63.9021 296.2785 14.97448612 76519Epoch: 2026-08-08T14:15Z
TLE epoch observation values (Epoch: 2026-08-08T14:15:20.776Z)
Latitude
0.00001°
Longitude
-59.29217°
Altitude
576.089 km
Speed
7.574 km/s
True Right ascension
07h 26m 35s
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
10:25:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.735 km
Perigee altitude
567.846 km
Semi-major axis
6,949.928 km
Eccentricity
0.00057
Inclination
97.6768°
RAAN
111.6475°
Arg. of periapsis
63.9021°
True anomaly
296.22017°
Mean anomaly
296.2785°
Eccentric anomaly
296.24934°
Mean motion
3.74604 °/min
Orbital period
96.1 mins
BSTAR
0.000079558
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-09 05:15:15.259Z | 27.56° NE | 2026-08-09 05:19:15.259Z | 115.644° SE | 33.6° | 2026-08-09 05:22:15.259Z | 168.81° S |
| 5 mins | 2026-08-09 16:04:15.259Z | 112.125° ESE | 2026-08-09 16:06:15.259Z | 71.82° E | 23.074° | 2026-08-09 16:09:15.259Z | 17.61° NNE |
| 4 mins | 2026-08-09 17:40:15.259Z | 237.826° WSW | 2026-08-09 17:41:15.259Z | 259.226° W | 21.403° | 2026-08-09 17:44:15.259Z | 313.842° NW |
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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