CSC-1, 58022
Orbit data source: Space-Track
CSC-1, 58022 is a payload satellite owned by ISIS BV (NL) in SSO that was launched on Mon, 09 Oct 2023 UTC via a VEGA 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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58022 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / NETHRelated business
Manufacturer
ISIS BV
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 6UXL, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.098 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 CSC-1
1 58022U 23155G 25307.90848346 .00003619 00000-0 23521-3 0 9997
2 58022 97.5659 15.7612 0006803 296.9530 63.1004 15.08625402113746Epoch: 2025-11-03T21:48Z
TLE epoch observation values (Epoch: 2025-11-03T21:48:12.970Z)
Latitude
0.00002°
Longitude
5.30405°
Altitude
541.342 km
Speed
7.593 km/s
True Right ascension
01h 03m 02s
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
03:53:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
542.092 km
Perigee altitude
532.683 km
Semi-major axis
6,915.524 km
Eccentricity
0.00068
Inclination
97.5659°
RAAN
15.7612°
Arg. of periapsis
296.953°
True anomaly
63.16995°
Mean anomaly
63.1004°
Eccentric anomaly
63.13517°
Mean motion
3.77403 °/min
Orbital period
95.39 mins
BSTAR
0.00023521
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Other satellites on launch #155 in the year 2023 (2023-10-09 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.CSC-1 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 | 2025-11-04 17:28:26.116Z | 15.258° NNE | 2025-11-04 17:31:26.116Z | 100.44° ESE | 44.617° | 2025-11-04 17:34:26.116Z | 188.864° SSW |
| 5 mins | 2025-11-05 04:12:26.116Z | 118.594° SE | 2025-11-05 04:14:26.116Z | 56.131° ENE | 29.965° | 2025-11-05 04:17:26.116Z | 6.082° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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