UVSQ-SAT NG, 63251
Orbit data source: Space-Track
UVSQ-SAT NG, 63251 is a payload satellite owned by LATMOS (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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63251 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
LATMOS
Mission
Operational Civil Earth Obs Sci
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.098 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 UVSQ-SAT NG
1 63251U 25052AT 25334.65142553 .00004764 00000-0 45143-3 0 9990
2 63251 97.7052 224.8692 0003569 138.0077 222.1417 14.94052627 38977Epoch: 2025-11-30T15:38Z
TLE epoch observation values (Epoch: 2025-11-30T15:38:03.165Z)
Latitude
-0.00007°
Longitude
-79.4062°
Altitude
590.205 km
Speed
7.564 km/s
True Right ascension
14h 59m 28s
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
02:13:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.812 km
Perigee altitude
579.844 km
Semi-major axis
6,960.465 km
Eccentricity
0.00036
Inclination
97.7052°
RAAN
224.8692°
Arg. of periapsis
138.0077°
True anomaly
222.11427°
Mean anomaly
222.1417°
Eccentric anomaly
222.12798°
Mean motion
3.73754 °/min
Orbital period
96.32 mins
BSTAR
0.00045143
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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.UVSQ-SAT NG 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-01 05:04:35.893Z | 42.457° NE | 2025-12-01 05:07:35.893Z | 105.129° ESE | 26.245° | 2025-12-01 05:10:35.893Z | 156.345° SSE |
| 4 mins | 2025-12-01 06:40:35.893Z | 327.541° NNW | 2025-12-01 06:42:35.893Z | 290.811° WNW | 19.418° | 2025-12-01 06:44:35.893Z | 254.917° W |
| 4 mins | 2025-12-01 15:54:35.893Z | 99.324° ESE | 2025-12-01 15:56:35.893Z | 62.977° ENE | 18.297° | 2025-12-01 15:58:35.893Z | 29.557° NE |
| 5 mins | 2025-12-01 17:29:35.893Z | 215.603° SW | 2025-12-01 17:31:35.893Z | 263.714° W | 28.125° | 2025-12-01 17:34:35.893Z | 322.188° 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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