FLTSATCOM 8 (USA 46), 20253
Orbit data source: Space-Track
FLTSATCOM 8 (USA 46), 20253 is a payload satellite owned by SPAWAR (US) in GEO that was launched on Mon, 25 Sep 1989 UTC via an ATLAS G CENTAUR 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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20253 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
TRW
Mission
Operational Defense Communications
Bus & Motor
FLTSATCOM, STAR 37FM
Mass
1,928 kg wet, 822 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl + 1 Dish + 2 Pan, 6.6 m
Radar Cross Section
11.171 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FLTSATCOM 8 (USA 46)
1 20253U 89077A 26093.63065931 -.00000369 00000-0 00000+0 0 9994
2 20253 12.4425 351.6111 0007954 357.8104 195.3548 1.00271974259814Epoch: 2026-04-03T15:08Z
TLE epoch observation values (Epoch: 2026-04-03T15:08:08.964Z)
Latitude
-2.81938°
Longitude
125.47693°
Altitude
35,818.992 km
Speed
3.072 km/s
True Right ascension
12h 17m 54s
True Declination
-2° 48' 60"
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
01:47:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,821.078 km
Perigee altitude
35,754.001 km
Semi-major axis
42,165.677 km
Eccentricity
0.0008
Inclination
12.4425°
RAAN
351.6111°
Arg. of periapsis
357.8104°
True anomaly
195.33069°
Mean anomaly
195.3548°
Eccentric anomaly
195.34274°
Mean motion
0.25067 °/min
Orbital period
1,436.14 mins
BSTAR
0
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Other satellites on launch #77 in the year 1989 (1989-09-25 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.FLTSATCOM 8 (USA 46) 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. |
|---|---|---|---|---|---|---|---|
| FLTSATCOM 8 (USA 46) is likely not visible in the next few days. |
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20253 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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