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: 1 day ago
TLE from 1 day ago
0 LEMUR 2 LEIA-PHILIP
1 63246U 25052AN 26259.48252750 .00002576 00000-0 22536-3 0 9993
2 63246 97.6681 149.8443 0002813 294.6547 65.4382 14.97608405 82332Epoch: 2026-09-16T11:34Z
TLE epoch observation values (Epoch: 2026-09-16T11:34:50.375Z)
Latitude
-0°
Longitude
-19.29908°
Altitude
576.528 km
Speed
7.573 km/s
True Right ascension
09h 59m 22s
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
08:17:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.25 km
Perigee altitude
569.34 km
Semi-major axis
6,949.432 km
Eccentricity
0.00028
Inclination
97.6681°
RAAN
149.8443°
Arg. of periapsis
294.6547°
True anomaly
65.46752°
Mean anomaly
65.4382°
Eccentric anomaly
65.45286°
Mean motion
3.74644 °/min
Orbital period
96.09 mins
BSTAR
0.00022536
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-09-17 16:33:36.104Z | 153.966° SSE | 2026-09-17 16:37:36.104Z | 73.447° E | 59.409° | 2026-09-17 16:41:36.104Z | 355.635° N |
| 7 mins | 2026-09-18 05:50:36.104Z | 4.734° NNE | 2026-09-18 05:53:36.104Z | 282.125° WNW | 68.808° | 2026-09-18 05:57:36.104Z | 201.756° SSW |
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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