GOES 14, 35491
Orbit data source: Space-Track
GOES 14, 35491 is a payload satellite owned by NOAA (US) in GEO that was launched on Sat, 27 Jun 2009 UTC via a DELTA 4M+(4,2) 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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35491 intel report (Beta)
GOES 14 details
| Identifier | |
| Orbit | GEO |
| Last TLE update | 18 hours ago |
| Origin | |
| Manufacturer | Boeing/ES |
| Mission | On reserve Civil Weather |
| Bus & Motor | HS-601, R-4D? |
| Mass | 3,209 kg wet, 1,543 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 1 Pan + 1 Ant, 8.2 m |
| Radar Cross Section | 14.281 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 18 hours ago
0 GOES 14
1 35491U 09033A 24348.13588244 -.00000053 00000-0 00000+0 0 9991
2 35491 0.2518 91.4053 0003044 131.5240 159.8474 1.00272799 56634Epoch: 2024-12-13T03:15Z
Definitive object data (Epoch: 2024-12-13T03:15:40.242Z)
| Latitude | -0.21383° |
| Longitude | -108.44629° |
| Altitude | 35,797.881 km |
| Speed | 3.074 km/s |
| True Right ascension | 01h 31m 06s |
| True Declination | 0° 12' 49" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -0.13371° |
| Longitude | 167.44124° |
| Altitude | 35,782.57 km |
| Speed | 3.075 km/s |
| Apparent Right ascension | 19h 52m 55s |
| Apparent Declination | -6° 22' 57" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 20:07:51 |
| Azimuth | 185.126° SSW |
| Elevation | 43.573° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 35,800.216 km |
| Perigee altitude | 35,774.546 km |
| Semi-major axis | 42,165.518 km |
| Eccentricity | 0.0003044 |
| Inclination | 0.2518° |
| RAAN | 91.4053° |
| Arg. of periapsis | 131.524° |
| True anomaly | 159.85941° |
| Mean anomaly | 159.8474° |
| Eccentric anomaly | 159.85341° |
| Mean motion | 0.25067 °/min |
| BSTAR | Unknown |
| Orbital period | 1436.14 mins |
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35491 neighbors
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Other satellites on launch #33 in the year 2009 (2009-06-27 UTC)
| GOES 14, 35491 |
| DELTA 4 R/B, 35492 |
GOES 14 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 | 2024-12-13 21:36:05.990Z | 185.124° SSW | 2024-12-14 13:45:05.990Z | 185.245° SSW | 34.774° | 2024-12-14 21:36:05.990Z | 185.111° SSW |
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