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, 1.8 m
Radar Cross Section
0.688 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 SPACEVAN-002
1 68424U 26067J 26263.40905425 .00003212 00000-0 15387-3 0 9998
2 68424 97.4622 220.5704 0003455 72.3592 287.8020 15.19649626 26397Epoch: 2026-09-20T09:49Z
TLE epoch observation values (Epoch: 2026-09-20T09:49:02.287Z)
Latitude
0.00001°
Longitude
74.00722°
Altitude
509.26 km
Speed
7.61 km/s
True Right ascension
14h 42m 16s
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
11:56:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.245 km
Perigee altitude
501.49 km
Semi-major axis
6,882.004 km
Eccentricity
0.00035
Inclination
97.4622°
RAAN
220.5704°
Arg. of periapsis
72.3592°
True anomaly
287.7643°
Mean anomaly
287.802°
Eccentric anomaly
287.78315°
Mean motion
3.80164 °/min
Orbital period
94.7 mins
BSTAR
0.00015387
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-20 21:00:43.619Z | 148.001° SSE | 2026-09-20 21:03:43.619Z | 62.02° ENE | 51.699° | 2026-09-20 21:06:43.619Z | 359.712° N |
| 6 mins | 2026-09-21 10:05:43.619Z | 14.672° NNE | 2026-09-21 10:07:43.619Z | 29.844° NE | 70.087° | 2026-09-21 10:11:43.619Z | 190.799° 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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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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