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: 2 days ago
TLE from 2 days ago
0 SPACEVAN-001
1 58295U 23174AR 26221.35558226 -.00000039 00000-0 87928-6 0 9998
2 58295 97.3999 320.5403 0006478 226.9043 133.1671 15.59064505154423Epoch: 2026-08-09T08:32Z
TLE epoch observation values (Epoch: 2026-08-09T08:32:02.307Z)
Latitude
-0.00009°
Longitude
-125.32306°
Altitude
396.508 km
Speed
7.671 km/s
True Right ascension
21h 22m 09s
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
16:31:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
391.66 km
Perigee altitude
382.894 km
Semi-major axis
6,765.414 km
Eccentricity
0.00065
Inclination
97.3999°
RAAN
320.5403°
Arg. of periapsis
226.9043°
True anomaly
133.22121°
Mean anomaly
133.1671°
Eccentric anomaly
133.19416°
Mean motion
3.90033 °/min
Orbital period
92.3 mins
BSTAR
8.7928e-7
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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 | 2026-08-11 06:52:33.610Z | 177.677° S | 2026-08-11 06:54:33.610Z | 210.179° SW | 39.088° | 2026-08-11 06:57:33.610Z | 340.5° N |
| 4 mins | 2026-08-11 19:38:33.610Z | 6.302° NNE | 2026-08-11 19:39:33.610Z | 352.084° N | 41.336° | 2026-08-11 19:42:33.610Z | 196.844° SSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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