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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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: 11 hours ago
TLE from 11 hours ago
0 PANDORE
1 63244U 25052AL 26264.92079357 .00001834 00000-0 17107-3 0 9990
2 63244 97.6754 154.3383 0003347 218.9216 141.1764 14.95415834 83067Epoch: 2026-09-21T22:05Z
TLE epoch observation values (Epoch: 2026-09-21T22:05:56.564Z)
Latitude
-0.00006°
Longitude
-177.94107°
Altitude
585.947 km
Speed
7.566 km/s
True Right ascension
10h 17m 21s
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
02:00:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.421 km
Perigee altitude
575.764 km
Semi-major axis
6,956.23 km
Eccentricity
0.00033
Inclination
97.6754°
RAAN
154.3383°
Arg. of periapsis
218.9216°
True anomaly
141.20044°
Mean anomaly
141.1764°
Eccentric anomaly
141.18842°
Mean motion
3.74095 °/min
Orbital period
96.23 mins
BSTAR
0.00017107
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-22 15:54:41.632Z | 115.347° SE | 2026-09-22 15:57:41.632Z | 61.315° ENE | 22.76° | 2026-09-22 15:59:41.632Z | 26.072° NE |
| 5 mins | 2026-09-22 17:30:41.632Z | 223.28° SW | 2026-09-22 17:32:41.632Z | 267.177° W | 26.974° | 2026-09-22 17:35:41.632Z | 319.505° NNW |
| 6 mins | 2026-09-23 05:11:41.632Z | 34.894° NE | 2026-09-23 05:14:41.632Z | 115.292° SE | 41.593° | 2026-09-23 05:17:41.632Z | 168.36° S |
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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