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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
CYL, 1.1 m
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 2
1 10061U 77048A   26256.41388154  .00000080  00000-0  00000+0 0  9996
2 10061   6.2165 292.7308 0011221  52.7536  23.8782  0.99395643 47151
Epoch: 2026-09-13T09:55Z
TLE epoch observation values (Epoch: 2026-09-13T09:55:59.365Z)
Latitude
6.0409°
Longitude
-132.05244°
Altitude
35,989.215 km
Speed
3.069 km/s
True Right ascension
00h 37m 24s
True Declination
6° 02' 05"
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
10:16:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,082.65 km
Perigee altitude
35,987.466 km
Semi-major axis
42,413.195 km
Eccentricity
0.00112
Inclination
6.2165°
RAAN
292.7308°
Arg. of periapsis
52.7536°
True anomaly
23.93032°
Mean anomaly
23.8782°
Eccentric anomaly
23.90425°
Mean motion
0.24848 °/min
Orbital period
1,448.81 mins
BSTAR
0
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