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: 10 hours ago
TLE from 10 hours ago
0 PANDORE
1 63244U 25052AL 26219.68533720 .00001225 00000-0 11645-3 0 9997
2 63244 97.6829 110.0219 0005759 37.9967 322.1659 14.95249869 76304Epoch: 2026-08-07T16:26Z
TLE epoch observation values (Epoch: 2026-08-07T16:26:53.134Z)
Latitude
-0.00002°
Longitude
-92.90698°
Altitude
581.481 km
Speed
7.571 km/s
True Right ascension
07h 20m 05s
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
16:45:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.615 km
Perigee altitude
574.602 km
Semi-major axis
6,956.745 km
Eccentricity
0.00058
Inclination
97.6829°
RAAN
110.0219°
Arg. of periapsis
37.9967°
True anomaly
322.1254°
Mean anomaly
322.1659°
Eccentric anomaly
322.14565°
Mean motion
3.74054 °/min
Orbital period
96.24 mins
BSTAR
0.00011645
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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 | 2026-08-08 05:51:36.679Z | 3.362° NNE | 2026-08-08 05:54:36.679Z | 312.476° NW | 40.609° | 2026-08-08 05:58:36.679Z | 205.717° SW |
| 6 mins | 2026-08-08 16:40:36.679Z | 158.393° S | 2026-08-08 16:43:36.679Z | 24.452° NE | 42.593° | 2026-08-08 16:46:36.679Z | 352.098° N |
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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