CO3D2, 64902
Orbit data source: Space-Track
CO3D2, 64902 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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64902 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: 11 hours ago
TLE from 11 hours ago
0 CO3D2
1 64902U 25156D 26171.37975280 .00003283 00000-0 15474-3 0 9998
2 64902 97.4328 249.9261 0001570 106.6316 253.5091 15.20193266 50011Epoch: 2026-06-20T09:06Z
TLE epoch observation values (Epoch: 2026-06-20T09:06:50.641Z)
Latitude
-0.00011°
Longitude
-155.3801°
Altitude
508.654 km
Speed
7.609 km/s
True Right ascension
16h 39m 42s
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
07:19:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.304 km
Perigee altitude
501.144 km
Semi-major axis
6,880.361 km
Eccentricity
0.00016
Inclination
97.4328°
RAAN
249.9261°
Arg. of periapsis
106.6316°
True anomaly
253.49185°
Mean anomaly
253.5091°
Eccentric anomaly
253.50047°
Mean motion
3.803 °/min
Orbital period
94.66 mins
BSTAR
0.00015474
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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.CO3D2 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 05:47:50.501Z | 214.439° SW | 2026-06-21 05:49:50.501Z | 280.172° WNW | 29.518° | 2026-06-21 05:51:50.501Z | 322.632° NNW |
| 4 mins | 2026-06-21 18:51:50.501Z | 327.667° NNW | 2026-06-21 18:53:50.501Z | 279.351° WNW | 22.331° | 2026-06-21 18:55:50.501Z | 240.58° WSW |
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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