CSO-3, 63156
Orbit data source: Space-Track
CSO-3, 63156 is a French payload satellite in SSO that was launched on Thu, 06 Mar 2025 UTC via an ARIANE 62 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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63156 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
Airbus/Toulouse
Mission
Operational spacecraft
Bus & Motor
ASTROSAT-100, AOCS
Mass
3,562 kg wet, ~2,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 6 months ago
TLE from 6 months ago
0 CSO-3
1 63156U 25044A 25073.57074855 .00000450 00000-0 17703-3 0 9994
2 63156 98.6061 14.9510 0001899 15.9635 344.1609 14.34023195 1122Epoch: 2025-03-14T13:41Z
TLE epoch observation values (Epoch: 2025-03-14T13:41:52.674Z)
Latitude
-0.00005°
Longitude
-2.9472°
Altitude
779.944 km
Speed
7.465 km/s
True Right ascension
00h 59m 48s
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
17:23:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.808 km
Perigee altitude
774.091 km
Semi-major axis
7,153.586 km
Eccentricity
0.00019
Inclination
98.6061°
RAAN
14.951°
Arg. of periapsis
15.9635°
True anomaly
344.15496°
Mean anomaly
344.1609°
Eccentric anomaly
344.15793°
Mean motion
3.58722 °/min
Orbital period
100.36 mins
BSTAR
0.00017703
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Other satellites on launch #44 in the year 2025 (2025-03-06 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.CSO-3 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-17 08:48:29.527Z | 19.113° NNE | 2025-09-17 08:53:29.527Z | 112.762° SE | 42.735° | 2025-09-17 08:57:29.527Z | 183.395° SSW |
| 4 mins | 2025-09-17 10:30:29.527Z | 318.188° NNW | 2025-09-17 10:32:29.527Z | 291.882° WNW | 14.448° | 2025-09-17 10:34:29.527Z | 267.888° W |
| 8 mins | 2025-09-17 20:05:29.527Z | 165.473° S | 2025-09-17 20:08:29.527Z | 167.474° S | 44.606° | 2025-09-17 20:13:29.527Z | 346.548° N |
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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