VIASAT 3-F3, 68893
Orbit data source: Space-Track
VIASAT 3-F3, 68893 is a payload satellite owned by ViaSat (US) that was launched on Wed, 29 Apr 2026 UTC via an FALCON HEAVY launch vehicle from the Air Force Eastern Test Range (AFETR). 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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68893 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Boeing/ES
Mission
Operational spacecraft
Bus & Motor
BSS-702MP+, R-4D
Mass
~6,500 kg wet, 3,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 VIASAT 3-F3
1 68893U 26096A 26154.08734587 -.00000121 00000-0 00000+0 0 9991
2 68893 1.6377 279.9090 0934378 180.9779 289.6284 1.17860811 452Epoch: 2026-06-03T02:05Z
TLE epoch observation values (Epoch: 2026-06-03T02:05:46.683Z)
Latitude
1.63077°
Longitude
97.06244°
Altitude
30,583.323 km
Speed
3.323 km/s
True Right ascension
01h 20m 13s
True Declination
1° 37' 44"
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
02:26:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,018.343 km
Perigee altitude
27,943.416 km
Semi-major axis
37,859.017 km
Eccentricity
0.09344
Inclination
1.6377°
RAAN
279.909°
Arg. of periapsis
180.9779°
True anomaly
279.19057°
Mean anomaly
289.6284°
Eccentric anomaly
284.44403°
Mean motion
0.29464 °/min
Orbital period
1,221.84 mins
BSTAR
0
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Other satellites on launch #96 in the year 2026 (2026-04-29 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.VIASAT 3-F3 Visibility
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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. |
|---|---|---|---|---|---|---|---|
| VIASAT 3-F3 is likely not visible in the next few days. |
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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