VEGA, 68430
Orbit data source: Space-Track
VEGA, 68430 is a Swedish payload satellite 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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68430 intel report (Beta)
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Identifier
Orbit
Country
SE / SWEDRelated business
None
Manufacturer
UNKSE
Mission
Operational spacecraft
Bus & Motor
CUBESAT 3U?, Unknown motor
Mass
~5 kg wet, ~5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 VEGA
1 68430U 26067Q 26171.34253855 .00005815 00000-0 28039-3 0 9998
2 68430 97.4497 129.7790 0001869 77.0476 283.0967 15.19087314 12426Epoch: 2026-06-20T08:13Z
TLE epoch observation values (Epoch: 2026-06-20T08:13:15.330Z)
Latitude
-0.00005°
Longitude
97.9066°
Altitude
511.394 km
Speed
7.608 km/s
True Right ascension
08h 39m 06s
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
16:35:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.853 km
Perigee altitude
504.28 km
Semi-major axis
6,883.704 km
Eccentricity
0.00019
Inclination
97.4497°
RAAN
129.779°
Arg. of periapsis
77.0476°
True anomaly
283.07584°
Mean anomaly
283.0967°
Eccentric anomaly
283.08627°
Mean motion
3.80023 °/min
Orbital period
94.73 mins
BSTAR
0.00028039
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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.VEGA 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 | 2026-06-22 09:48:03.339Z | 29.431° NE | 2026-06-22 09:51:03.339Z | 121.305° SE | 35.442° | 2026-06-22 09:54:03.339Z | 174.063° S |
| 4 mins | 2026-06-22 22:01:03.339Z | 224.607° SW | 2026-06-22 22:03:03.339Z | 271.624° WNW | 22.241° | 2026-06-22 22:05:03.339Z | 311.785° NW |
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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