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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10061 intel report (Beta)
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Edit Public Description
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
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 GOES 2
1 10061U 77048A 25350.12884809 -.00000109 00000-0 00000-0 0 9990
2 10061 6.8560 294.8686 0012792 39.2150 159.0864 0.99400880 44457Epoch: 2025-12-16T03:05Z
TLE epoch observation values (Epoch: 2025-12-16T03:05:32.474Z)
Latitude
-2.15135°
Longitude
1.66913°
Altitude
36,082.829 km
Speed
3.062 km/s
True Right ascension
08h 52m 17s
True Declination
-2° 08' 57"
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
21:38:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,087.817 km
Perigee altitude
35,979.311 km
Semi-major axis
42,411.701 km
Eccentricity
0.00128
Inclination
6.856°
RAAN
294.8686°
Arg. of periapsis
39.215°
True anomaly
159.13865°
Mean anomaly
159.0864°
Eccentric anomaly
159.11253°
Mean motion
0.24849 °/min
Orbital period
1,448.73 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. |
|---|---|---|---|---|---|---|---|
| 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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