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 spacecraft
Bus & Motor
MP42, Unknown motor
Mass
125 kg wet, ~120 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 SPACEVAN-002
1 68424U 26067J 26171.44013822 .00002520 00000-0 12656-3 0 9998
2 68424 97.4521 129.8233 0003444 64.6116 295.5474 15.18187534 12430Epoch: 2026-06-20T10:33Z
TLE epoch observation values (Epoch: 2026-06-20T10:33:47.942Z)
Latitude
-0.00003°
Longitude
62.71881°
Altitude
513.382 km
Speed
7.608 km/s
True Right ascension
08h 39m 17s
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
13:48:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.66 km
Perigee altitude
505.917 km
Semi-major axis
6,886.426 km
Eccentricity
0.00034
Inclination
97.4521°
RAAN
129.8233°
Arg. of periapsis
64.6116°
True anomaly
295.51179°
Mean anomaly
295.5474°
Eccentric anomaly
295.52959°
Mean motion
3.79798 °/min
Orbital period
94.79 mins
BSTAR
0.00012656
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 10:35:30.859Z | 343.202° N | 2026-06-22 10:37:30.859Z | 287.276° WNW | 31.724° | 2026-06-22 10:40:30.859Z | 221.109° SW |
| 6 mins | 2026-06-22 21:13:30.859Z | 162.159° S | 2026-06-22 21:16:30.859Z | 12.482° NNE | 42.765° | 2026-06-22 21:19:30.859Z | 350.635° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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