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: 7 hours ago
TLE from 7 hours ago
0 LEMUR 2 LEIA-PHILIP
1 63246U 25052AN 26296.96316381 .00003401 00000-0 29428-3 0 9993
2 63246 97.6640 186.6424 0004555 141.8804 218.2741 14.97820554 87949Epoch: 2026-10-23T23:06Z
TLE epoch observation values (Epoch: 2026-10-23T23:06:57.353Z)
Latitude
-0.00003°
Longitude
167.52726°
Altitude
579.171 km
Speed
7.57 km/s
True Right ascension
12h 26m 34s
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
01:28:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.804 km
Perigee altitude
567.473 km
Semi-major axis
6,948.775 km
Eccentricity
0.00046
Inclination
97.664°
RAAN
186.6424°
Arg. of periapsis
141.8804°
True anomaly
218.24178°
Mean anomaly
218.2741°
Eccentric anomaly
218.25794°
Mean motion
3.74697 °/min
Orbital period
96.08 mins
BSTAR
0.00029428
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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 | 2026-10-24 16:52:16.062Z | 170.435° S | 2026-10-24 16:56:16.062Z | 322.814° NNW | 69.22° | 2026-10-24 16:59:16.062Z | 345.063° N |
| 6 mins | 2026-10-25 06:09:16.062Z | 346.837° N | 2026-10-25 06:11:16.062Z | 303.028° NW | 39.014° | 2026-10-25 06:15:16.062Z | 218.857° SW |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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