PVCC, 58025
Orbit data source: Space-Track
PVCC, 58025 is a payload satellite owned by ESA (BE) 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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58025 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
BE / BELRelated business
Manufacturer
Aerospacelab
Mission
Operational Civil Imaging
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 0.4 m
Radar Cross Section
0.150 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 PVCC
1 58025U 23155K 25307.94437082 .00008783 00000-0 51096-3 0 9990
2 58025 97.5971 20.3618 0004755 173.3872 186.7422 15.12285838113897Epoch: 2025-11-03T22:39Z
TLE epoch observation values (Epoch: 2025-11-03T22:39:53.638Z)
Latitude
-0.00005°
Longitude
-3.05017°
Altitude
535.568 km
Speed
7.593 km/s
True Right ascension
01h 21m 26s
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
03:53:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.498 km
Perigee altitude
522.932 km
Semi-major axis
6,904.352 km
Eccentricity
0.00048
Inclination
97.5971°
RAAN
20.3618°
Arg. of periapsis
173.3872°
True anomaly
186.73581°
Mean anomaly
186.7422°
Eccentric anomaly
186.739°
Mean motion
3.7832 °/min
Orbital period
95.16 mins
BSTAR
0.00051096
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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.PVCC 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-04 18:17:25.150Z | 349.023° N | 2025-11-04 18:19:25.150Z | 305.495° NW | 32.056° | 2025-11-04 18:22:25.150Z | 223.513° SW |
| 6 mins | 2025-11-05 04:58:25.150Z | 164.571° S | 2025-11-05 05:00:25.150Z | 156.123° SSE | 42.797° | 2025-11-05 05:04:25.150Z | 348.972° N |
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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