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: 12 hours ago
TLE from 12 hours ago
0 PANDORE
1 63244U 25052AL 26049.59269874 .00003593 00000-0 33984-3 0 9994
2 63244 97.7052 303.2193 0003482 216.8886 143.2095 14.94279463 50893Epoch: 2026-02-18T14:13Z
TLE epoch observation values (Epoch: 2026-02-18T14:13:29.171Z)
Latitude
-0.00002°
Longitude
-58.70837°
Altitude
589.599 km
Speed
7.564 km/s
True Right ascension
20h 12m 52s
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
04:42:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.047 km
Perigee altitude
579.2 km
Semi-major axis
6,959.76 km
Eccentricity
0.00035
Inclination
97.7052°
RAAN
303.2193°
Arg. of periapsis
216.8886°
True anomaly
143.23339°
Mean anomaly
143.2095°
Eccentric anomaly
143.22144°
Mean motion
3.73811 °/min
Orbital period
96.31 mins
BSTAR
0.00033984
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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 | 2026-02-19 05:15:29.606Z | 28.639° NE | 2026-02-19 05:18:29.606Z | 78.741° E | 33.245° | 2026-02-19 05:22:29.606Z | 169.169° S |
| 5 mins | 2026-02-19 16:05:29.606Z | 115.235° SE | 2026-02-19 16:07:29.606Z | 76.729° E | 23.92° | 2026-02-19 16:10:29.606Z | 19.073° NNE |
| 4 mins | 2026-02-19 17:41:29.606Z | 231.778° WSW | 2026-02-19 17:43:29.606Z | 273.246° WNW | 21.184° | 2026-02-19 17:45:29.606Z | 308.589° NW |
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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