PANDORE, 63244
Orbit data source: Space-Track
PANDORE, 63244 is a payload satellite owned by U-Space (FR) 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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63244 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
U-Space
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~16 kg wet, ~16 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.155 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 PANDORE
1 63244U 25052AL 25301.65063391 .00005776 00000-0 55939-3 0 9996
2 63244 97.7105 192.4185 0003206 241.8943 118.1952 14.93101438 34033Epoch: 2025-10-28T15:36Z
TLE epoch observation values (Epoch: 2025-10-28T15:36:54.769Z)
Latitude
-0.00013°
Longitude
-79.04476°
Altitude
592.373 km
Speed
7.563 km/s
True Right ascension
12h 49m 40s
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
15:48:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.519 km
Perigee altitude
583.054 km
Semi-major axis
6,963.424 km
Eccentricity
0.00032
Inclination
97.7105°
RAAN
192.4185°
Arg. of periapsis
241.8943°
True anomaly
118.22757°
Mean anomaly
118.1952°
Eccentric anomaly
118.21139°
Mean motion
3.73516 °/min
Orbital period
96.38 mins
BSTAR
0.00055939
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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.PANDORE 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 | 2025-10-29 05:03:09.263Z | 35.494° NE | 2025-10-29 05:07:09.263Z | 108.855° ESE | 25.672° | 2025-10-29 05:10:09.263Z | 156.768° SSE |
| 4 mins | 2025-10-29 06:40:09.263Z | 326.637° NNW | 2025-10-29 06:42:09.263Z | 288.972° WNW | 19.919° | 2025-10-29 06:44:09.263Z | 253.361° W |
| 6 mins | 2025-10-29 17:29:09.263Z | 211.16° SW | 2025-10-29 17:31:09.263Z | 254.409° W | 28.297° | 2025-10-29 17:35:09.263Z | 327.659° NNW |
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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