SPACEVAN-001, 58295
Orbit data source: Space-Track
SPACEVAN-001, 58295 is a payload satellite owned by Exotrail (FR) in SSO that was launched on Sat, 11 Nov 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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58295 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Technology
Bus & Motor
MP42, Unknown motor
Mass
125 kg wet, ~120 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.8 m
Radar Cross Section
0.688 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 SPACEVAN-001
1 58295U 23174AR 25285.74055047 .00000783 00000-0 13124-4 0 9993
2 58295 97.4054 8.6464 0007836 311.9704 48.0882 15.55174926107640Epoch: 2025-10-12T17:46Z
TLE epoch observation values (Epoch: 2025-10-12T17:46:23.560Z)
Latitude
-0.00002°
Longitude
80.49489°
Altitude
401.235 km
Speed
7.672 km/s
True Right ascension
00h 34m 35s
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
07:04:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
403.873 km
Perigee altitude
393.253 km
Semi-major axis
6,776.7 km
Eccentricity
0.00078
Inclination
97.4054°
RAAN
8.6464°
Arg. of periapsis
311.9704°
True anomaly
48.15507°
Mean anomaly
48.0882°
Eccentric anomaly
48.12163°
Mean motion
3.89059 °/min
Orbital period
92.53 mins
BSTAR
0.000013124
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Other satellites on launch #174 in the year 2023 (2023-11-11 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.SPACEVAN-001 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 | 2025-10-17 18:47:10.494Z | 355.953° N | 2025-10-17 18:49:10.494Z | 290.736° WNW | 37.801° | 2025-10-17 18:52:10.494Z | 208.385° SW |
| 4 mins | 2025-10-18 05:11:10.494Z | 119.04° SE | 2025-10-18 05:13:10.494Z | 58.876° ENE | 23.996° | 2025-10-18 05:15:10.494Z | 15.437° 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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