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GOES 1 (SMS-C), 8366

Orbit data source: Space-Track

GOES 1 (SMS-C), 8366 is a payload satellite owned by NOAA (US) in GEO that was launched on Thu, 16 Oct 1975 UTC via a DELTA 2914 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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Identifier
8366, 1975-100A
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
Ae Ford WDL
Mission
Non-operational spacecraft
Bus & Motor
SMS, SVM-5
Mass
~612 kg wet, ~277 kg dry
Launch date (UTC)
1975-10-16 (50 years ago)
Launch vehicle
DELTA 2914
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 GOES 1 (SMS-C)
1 08366U 75100A   26089.08901348  .00000005  00000-0  00000-0 0  9999
2 08366   4.8094 278.4458 0004802   2.4073 175.0980  1.00243251184278
Epoch: 2026-03-30T02:08Z
TLE epoch observation values (Epoch: 2026-03-30T02:08:10.764Z)
Latitude
0.18111°
Longitude
-123.53325°
Altitude
35,814.149 km
Speed
3.073 km/s
True Right ascension
06h 23m 59s
True Declination
0° 10' 51"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
08:21:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,815.907 km
Perigee altitude
35,775.403 km
Semi-major axis
42,173.792 km
Eccentricity
0.00048
Inclination
4.8094°
RAAN
278.4458°
Arg. of periapsis
2.4073°
True anomaly
175.1027°
Mean anomaly
175.098°
Eccentric anomaly
175.10035°
Mean motion
0.2506 °/min
Orbital period
1,436.56 mins
BSTAR
0
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