SPACEVAN-002, 68424
Orbit data source: Space-Track
SPACEVAN-002, 68424 is a payload satellite owned by Exotrail (FR) in SSO that was launched on Mon, 30 Mar 2026 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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68424 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, 1.5 m
Radar Cross Section
0.688 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 SPACEVAN-002
1 68424U 26067J 26217.50300928 .00007962 00000-0 38658-3 0 9997
2 68424 97.4546 175.2303 0001298 145.6366 214.4952 15.18732798 19427Epoch: 2026-08-05T12:04Z
TLE epoch observation values (Epoch: 2026-08-05T12:04:20.001Z)
Latitude
-0.00009°
Longitude
40.09049°
Altitude
513.494 km
Speed
7.607 km/s
True Right ascension
11h 40m 55s
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
19:00:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.533 km
Perigee altitude
505.745 km
Semi-major axis
6,884.776 km
Eccentricity
0.00013
Inclination
97.4546°
RAAN
175.2303°
Arg. of periapsis
145.6366°
True anomaly
214.48678°
Mean anomaly
214.4952°
Eccentric anomaly
214.49099°
Mean motion
3.79934 °/min
Orbital period
94.75 mins
BSTAR
0.00038658
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Other satellites on launch #67 in the year 2026 (2026-03-30 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-002 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 | 2026-08-06 09:13:05.769Z | 60.332° ENE | 2026-08-06 09:15:05.769Z | 97.987° ESE | 16.478° | 2026-08-06 09:17:05.769Z | 132.906° SE |
| 4 mins | 2026-08-06 10:47:05.769Z | 331.738° NNW | 2026-08-06 10:49:05.769Z | 281.191° WNW | 24.769° | 2026-08-06 10:51:05.769Z | 238.639° WSW |
| 5 mins | 2026-08-06 21:25:05.769Z | 177.544° S | 2026-08-06 21:27:05.769Z | 235.906° WSW | 43.371° | 2026-08-06 21:30:05.769Z | 342.068° N |
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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