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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 Civil Weather
Bus & Motor
SMS, SVM-5
Mass
624 kg wet, ~277 kg dry
Launch date (UTC)
1977-06-16 (48 years ago)
Launch vehicle
DELTA 2914
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 1.3 m
Radar Cross Section
5.298 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 GOES 2
1 10061U 77048A   25258.49938223 -.00000190  00000-0  00000-0 0  9997
2 10061   7.0775 295.6120 0010708  43.5559 125.6050  0.99396424 43549
Epoch: 2025-09-15T11:59Z
TLE epoch observation values (Epoch: 2025-09-15T11:59:06.624Z)
Latitude
1.3059°
Longitude
-69.51328°
Altitude
36,059.68 km
Speed
3.064 km/s
True Right ascension
06h 59m 52s
True Declination
1° 18' 17"
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
23:04:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,080.246 km
Perigee altitude
35,989.415 km
Semi-major axis
42,412.967 km
Eccentricity
0.00107
Inclination
7.0775°
RAAN
295.612°
Arg. of periapsis
43.5559°
True anomaly
125.70469°
Mean anomaly
125.605°
Eccentric anomaly
125.65485°
Mean motion
0.24848 °/min
Orbital period
1,448.8 mins
BSTAR
0
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