CO3D1, 64903
Orbit data source: Space-Track
CO3D1, 64903 is a payload satellite owned by CNES (FR) in SSO that was launched on Sat, 26 Jul 2025 UTC via a VEGA C launch vehicle from the French Guiana (FRGUI). 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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64903 intel report (Beta)
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Identifier
Orbit
Country
FRRelated business
Manufacturer
Airbus/Toulouse
Mission
Operational Civil Science
Bus & Motor
ASTROBUS-SE, Unknown motor
Mass
285 kg wet, 285 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.9 m
Radar Cross Section
1.001 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 CO3D1
1 64903U 25156E 26171.05079051 .00004283 00000-0 20076-3 0 9990
2 64903 97.4325 249.6020 0001352 114.2620 245.8756 15.20215547 49961Epoch: 2026-06-20T01:13Z
TLE epoch observation values (Epoch: 2026-06-20T01:13:08.300Z)
Latitude
-0.00005°
Longitude
-36.95355°
Altitude
508.66 km
Speed
7.609 km/s
True Right ascension
16h 38m 24s
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
07:21:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.087 km
Perigee altitude
501.226 km
Semi-major axis
6,880.294 km
Eccentricity
0.00014
Inclination
97.4325°
RAAN
249.602°
Arg. of periapsis
114.262°
True anomaly
245.86146°
Mean anomaly
245.8756°
Eccentric anomaly
245.86853°
Mean motion
3.80306 °/min
Orbital period
94.66 mins
BSTAR
0.00020076
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Other satellites on launch #156 in the year 2025 (2025-07-26 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.CO3D1 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 | 2026-06-21 05:47:36.663Z | 207.725° SW | 2026-06-21 05:49:36.663Z | 263.739° W | 30.338° | 2026-06-21 05:52:36.663Z | 327.629° NNW |
| 4 mins | 2026-06-21 18:52:36.663Z | 316.014° NNW | 2026-06-21 18:53:36.663Z | 290.541° WNW | 22.579° | 2026-06-21 18:56:36.663Z | 234.501° WSW |
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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