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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: 8 hours ago

TLE from 8 hours ago
0 GOES 1 (SMS-C)
1 08366U 75100A   25364.53548720 -.00000016  00000-0  00000-0 0  9998
2 08366   5.0366 279.5522 0006298 346.0639 274.8556  1.00227911183375
Epoch: 2025-12-30T12:51Z
TLE epoch observation values (Epoch: 2025-12-30T12:51:06.094Z)
Latitude
-4.98062°
Longitude
-111.64185°
Altitude
35,796.995 km
Speed
3.074 km/s
True Right ascension
12h 01m 24s
True Declination
-4° 58' 32"
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
20:46:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,826.521 km
Perigee altitude
35,773.393 km
Semi-major axis
42,178.094 km
Eccentricity
0.00063
Inclination
5.0366°
RAAN
279.5522°
Arg. of periapsis
346.0639°
True anomaly
274.78368°
Mean anomaly
274.8556°
Eccentric anomaly
274.81964°
Mean motion
0.25056 °/min
Orbital period
1,436.78 mins
BSTAR
0
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