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). Payloads include a variety of satellites, spacecraft, and rockets 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)
GOES 2 details
| Identifier | |
| Orbit | GEO |
| Last TLE update | 3 days ago |
| Origin | |
| Manufacturer | Ford Ae |
| Mission | Non-operational Civil Weather |
| Bus & Motor | SMS, SVM-5 |
| Mass | 624 kg wet, ~277 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Cyl, 2.6 m |
| Radar Cross Section | 5.298 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 3 days ago
0 GOES 2
1 10061U 77048A 25023.17135333 -.00000218 00000-0 00000-0 0 9994
2 10061 7.6327 297.6769 0012979 36.4421 161.2196 0.99398508 41203Epoch: 2025-01-23T04:06Z
Definitive object data (Epoch: 2025-01-23T04:06:44.927Z)
| Latitude | -2.30143° |
| Longitude | -49.19039° |
| Altitude | 36,085.299 km |
| Speed | 3.062 km/s |
| True Right ascension | 09h 00m 59s |
| True Declination | -2° 17' 57" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 5.65542° |
| Longitude | 161.03104° |
| Altitude | 35,978.497 km |
| Speed | 3.07 km/s |
| Apparent Right ascension | 23h 23m 10s |
| Apparent Declination | 0° 08' 44" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 19:51:24 |
| Azimuth | 115.74° SE |
| Elevation | 27.635° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 36,089.281 km |
| Perigee altitude | 35,979.187 km |
| Semi-major axis | 42,412.371 km |
| Eccentricity | 0.0012979 |
| Inclination | 7.6327° |
| RAAN | 297.6769° |
| Arg. of periapsis | 36.4421° |
| True anomaly | 161.26741° |
| Mean anomaly | 161.2196° |
| Eccentric anomaly | 161.24351° |
| Mean motion | 0.24849 °/min |
| BSTAR | Unknown |
| Orbital period | 1448.77 mins |
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10061 neighbors
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Other satellites on launch #48 in the year 1977 (1977-06-16 UTC)
| GOES 2, 10061 |
| DELTA 1 R/B(1), 10062 |
| DELTA 1 DEB, 10063 (Decayed) |
| DELTA 1 DEB, 10067 (Decayed) |
| DELTA 1 DEB, 10075 (Decayed) |
| DELTA 1 R/B(2), 10409 (Decayed) |
| GOES 2 AKM, 20799 |
GOES 2 Visibility forecast
Observer location: undefined°, undefined
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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-01-25 18:30:37.083Z | 115.756° SE | 2025-01-26 18:30:37.083Z | 118.763° SE | 26.418° | 2025-01-26 18:30:37.083Z | 118.763° SE |
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