VIASAT 3-F1, 56370
Orbit data source: Space-Track
VIASAT 3-F1, 56370 is a payload satellite owned by ViaSat (US) in GEO that was launched on Mon, 01 May 2023 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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56370 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Boeing/ES
Mission
Partially operational Commercial Communications
Bus & Motor
BSS-702MP+, R-4D
Mass
6,418 kg wet, 3,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan + 1 Rod + 1 Dish, 22.0 m
Radar Cross Section
58.453 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 VIASAT 3-F1
1 56370U 23060A 25364.37512642 .00000000 00000-0 00000-0 0 9992
2 56370 0.0173 9.4906 0000334 352.2526 143.4013 1.00271122 9749Epoch: 2025-12-30T09:00Z
TLE epoch observation values (Epoch: 2025-12-30T09:00:10.922Z)
Latitude
0.02677°
Longitude
-88.96144°
Altitude
35,787.393 km
Speed
3.075 km/s
True Right ascension
09h 40m 34s
True Declination
0° 01' 36"
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
22:57:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,789.26 km
Perigee altitude
35,786.443 km
Semi-major axis
42,165.988 km
Eccentricity
0.00003
Inclination
0.0173°
RAAN
9.4906°
Arg. of periapsis
352.2526°
True anomaly
143.40358°
Mean anomaly
143.4013°
Eccentric anomaly
143.40244°
Mean motion
0.25067 °/min
Orbital period
1,436.16 mins
BSTAR
0
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Other satellites on launch #60 in the year 2023 (2023-05-01 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-F1 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-12-30 23:19:42.530Z | 155.697° SSE | 2025-12-31 06:57:42.530Z | 155.67° SSE | 33.236° | 2025-12-31 23:19:42.530Z | 155.695° SSE |
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56370 neighbors
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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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