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: 9 hours ago
TLE from 9 hours ago
0 PANDORE
1 63244U 25052AL 26104.16025220 .00001466 00000-0 14034-3 0 9996
2 63244 97.6973 356.7510 0006056 58.2996 301.8814 14.94686068 59040Epoch: 2026-04-14T03:50Z
TLE epoch observation values (Epoch: 2026-04-14T03:50:45.790Z)
Latitude
-0.00003°
Longitude
96.71972°
Altitude
584.17 km
Speed
7.569 km/s
True Right ascension
23h 47m 00s
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
19:15:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.574 km
Perigee altitude
576.146 km
Semi-major axis
6,958.497 km
Eccentricity
0.00061
Inclination
97.6973°
RAAN
356.751°
Arg. of periapsis
58.2996°
True anomaly
301.82245°
Mean anomaly
301.8814°
Eccentric anomaly
301.85193°
Mean motion
3.73913 °/min
Orbital period
96.28 mins
BSTAR
0.00014034
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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 | 2026-04-14 16:48:51.055Z | 166.994° S | 2026-04-14 16:52:51.055Z | 335.003° NNW | 44.858° | 2026-04-14 16:55:51.055Z | 347.227° N |
| 6 mins | 2026-04-15 06:07:51.055Z | 347.628° N | 2026-04-15 06:09:51.055Z | 300.457° NW | 33.937° | 2026-04-15 06:13:51.055Z | 216.635° 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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