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 an SPECTRUM 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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10061 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Ford Ae
Mission
Non-operational spacecraft
Bus & Motor
SMS, SVM-5
Mass
624 kg wet, ~277 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GOES 2
1 10061U 77048A 26271.61524079 -.00000115 00000-0 00000-0 0 9994
2 10061 6.1807 292.6253 0011357 51.5227 64.8946 0.99401711 47303Epoch: 2026-09-28T14:45Z
TLE epoch observation values (Epoch: 2026-09-28T14:45:56.804Z)
Latitude
5.51481°
Longitude
-179.59765°
Altitude
36,010.613 km
Speed
3.067 km/s
True Right ascension
03h 17m 07s
True Declination
5° 30' 33"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
08:50:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,081.499 km
Perigee altitude
35,985.165 km
Semi-major axis
42,411.469 km
Eccentricity
0.00114
Inclination
6.1807°
RAAN
292.6253°
Arg. of periapsis
51.5227°
True anomaly
65.01252°
Mean anomaly
64.8946°
Eccentric anomaly
64.95355°
Mean motion
0.2485 °/min
Orbital period
1,448.72 mins
BSTAR
0
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Other satellites on launch #48 in the year 1977 (1977-06-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GOES 2 Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| GOES 2 is likely not visible in the next few days. |
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10061 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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