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GOES 2, 10061

Orbit data source: Space-Track

GOES 2, 10061 is a payload satellite owned by NOAA (US) in GEO that was launched on Thu, 16 Jun 1977 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
10061, 1977-048A
Orbit
GEO
Country
Flag of USUS
Related business
Manufacturer
Ford Ae
Mission
Non-operational spacecraft
Bus & Motor
SMS, SVM-5
Mass
624 kg wet, ~277 kg dry
Launch date (UTC)
1977-06-16 (49 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: 9 hours ago

TLE from 9 hours ago
0 GOES 2
1 10061U 77048A   26002.23786352 -.00000224  00000-0  00000-0 0  9999
2 10061   6.8142 294.7236 0013179  40.7810 160.0923  0.99398263 44621
Epoch: 2026-01-02T05:42Z
TLE epoch observation values (Epoch: 2026-01-02T05:42:31.408Z)
Latitude
-2.41279°
Longitude
-52.00468°
Altitude
36,085.643 km
Speed
3.062 km/s
True Right ascension
09h 02m 01s
True Declination
-2° 24' 37"
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
14:16:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,090.204 km
Perigee altitude
35,978.414 km
Semi-major axis
42,412.446 km
Eccentricity
0.00132
Inclination
6.8142°
RAAN
294.7236°
Arg. of periapsis
40.781°
True anomaly
160.14364°
Mean anomaly
160.0923°
Eccentric anomaly
160.11798°
Mean motion
0.24849 °/min
Orbital period
1,448.77 mins
BSTAR
0
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