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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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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 SPACEVAN-001
1 58295U 23174AR 26285.29565057 .00043498 00000-0 49214-3 0 9999
2 58295 97.4018 27.1956 0006295 3.0137 357.1158 15.62300811164396Epoch: 2026-10-12T07:05Z
TLE epoch observation values (Epoch: 2026-10-12T07:05:44.209Z)
Latitude
0.00001°
Longitude
-100.11473°
Altitude
379.91 km
Speed
7.684 km/s
True Right ascension
01h 48m 46s
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
19:35:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
382.175 km
Perigee altitude
373.669 km
Semi-major axis
6,756.059 km
Eccentricity
0.00063
Inclination
97.4018°
RAAN
27.1956°
Arg. of periapsis
3.0137°
True anomaly
357.11217°
Mean anomaly
357.1158°
Eccentric anomaly
357.11398°
Mean motion
3.90844 °/min
Orbital period
92.11 mins
BSTAR
0.00049214
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-10-13 06:18:07.400Z | 114.921° SE | 2026-10-13 06:20:07.400Z | 67.369° ENE | 19.563° | 2026-10-13 06:22:07.400Z | 23.5° NE |
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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