CO3D4, 64901
Orbit data source: Space-Track
CO3D4, 64901 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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64901 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: 13 hours ago
TLE from 13 hours ago
0 CO3D4
1 64901U 25156C 26171.41309958 .00000218 00000-0 13182-4 0 9995
2 64901 97.4331 250.0596 0000098 241.9959 118.1266 15.20197278 50026Epoch: 2026-06-20T09:54Z
TLE epoch observation values (Epoch: 2026-06-20T09:54:51.803Z)
Latitude
-0.00006°
Longitude
-167.28432°
Altitude
508.367 km
Speed
7.61 km/s
True Right ascension
16h 40m 14s
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
10:18:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.279 km
Perigee altitude
502.144 km
Semi-major axis
6,880.349 km
Eccentricity
0.00001
Inclination
97.4331°
RAAN
250.0596°
Arg. of periapsis
241.9959°
True anomaly
118.12759°
Mean anomaly
118.1266°
Eccentric anomaly
118.1271°
Mean motion
3.80301 °/min
Orbital period
94.66 mins
BSTAR
0.000013182
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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.CO3D4 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 05:00:15.288Z | 146.984° SSE | 2026-06-21 05:03:15.288Z | 64.022° ENE | 37.394° | 2026-06-21 05:06:15.288Z | 0.549° NNE |
| 5 mins | 2026-06-21 18:05:15.288Z | 16.725° NNE | 2026-06-21 18:07:15.288Z | 75.432° E | 44.472° | 2026-06-21 18:10:15.288Z | 188.647° 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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