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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 LEMUR 2 LEIA-PHILIP
1 63246U 25052AN 26126.43424797 .00001592 00000-0 14269-3 0 9994
2 63246 97.6871 19.0820 0004314 29.9703 330.1766 14.97193750 62429Epoch: 2026-05-06T10:25Z
TLE epoch observation values (Epoch: 2026-05-06T10:25:19.024Z)
Latitude
0.00005°
Longitude
-1.54207°
Altitude
576.02 km
Speed
7.574 km/s
True Right ascension
01h 16m 19s
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
12:20:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.579 km
Perigee altitude
569.582 km
Semi-major axis
6,950.717 km
Eccentricity
0.00043
Inclination
97.6871°
RAAN
19.082°
Arg. of periapsis
29.9703°
True anomaly
330.152°
Mean anomaly
330.1766°
Eccentric anomaly
330.1643°
Mean motion
3.7454 °/min
Orbital period
96.12 mins
BSTAR
0.00014269
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-07 04:39:30.396Z | 58.322° ENE | 2026-05-07 04:41:30.396Z | 89.643° E | 15.368° | 2026-05-07 04:43:30.396Z | 122.669° SE |
| 6 mins | 2026-05-07 06:14:30.396Z | 346.284° N | 2026-05-07 06:17:30.396Z | 271.479° WNW | 30.286° | 2026-05-07 06:20:30.396Z | 222.314° SW |
| 7 mins | 2026-05-07 17:01:30.396Z | 178.456° S | 2026-05-07 17:04:30.396Z | 259.539° W | 42.523° | 2026-05-07 17:08:30.396Z | 342.003° N |
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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