CO3D3, 64900
Orbit data source: Space-Track
CO3D3, 64900 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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64900 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: 9 hours ago
TLE from 9 hours ago
0 CO3D3
1 64900U 25156B 26171.47876997 .00003433 00000-0 16165-3 0 9997
2 64900 97.4324 250.1245 0001587 126.6035 233.5346 15.20194218 50030Epoch: 2026-06-20T11:29Z
TLE epoch observation values (Epoch: 2026-06-20T11:29:25.725Z)
Latitude
-0.00005°
Longitude
169.07451°
Altitude
508.994 km
Speed
7.609 km/s
True Right ascension
16h 40m 29s
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
07:20:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.313 km
Perigee altitude
501.129 km
Semi-major axis
6,880.358 km
Eccentricity
0.00016
Inclination
97.4324°
RAAN
250.1245°
Arg. of periapsis
126.6035°
True anomaly
233.51998°
Mean anomaly
233.5346°
Eccentric anomaly
233.52729°
Mean motion
3.803 °/min
Orbital period
94.66 mins
BSTAR
0.00016165
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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.CO3D3 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 | 2026-06-21 05:00:04.655Z | 146.534° SSE | 2026-06-21 05:03:04.655Z | 61.766° ENE | 37.145° | 2026-06-21 05:06:04.655Z | 0.513° NNE |
| 5 mins | 2026-06-21 18:05:04.655Z | 17.117° NNE | 2026-06-21 18:07:04.655Z | 88.579° E | 44.498° | 2026-06-21 18:10:04.655Z | 188.468° SSW |
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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