INTELSAT 515, 19772
Orbit data source: Space-Track
INTELSAT 515, 19772 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Fri, 27 Jan 1989 UTC via an ARIANE 2 launch vehicle from the French Guiana (FRGUI). 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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19772 intel report (Beta)
INTELSAT 515 details
Identifier | |
Orbit | GEO |
Last TLE update | 11 hours ago |
Origin | |
Manufacturer | Ford Ae |
Mission | Non-operational Civil Communications |
Bus & Motor | FS INTELSAT 5, STAR 37XF |
Mass | 1,981 kg wet, 884 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Hex Poly + 2 Pan, 15.9 m |
Radar Cross Section | 18.961 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 11 hours ago
0 INTELSAT 515
1 19772U 89006A 24361.35819081 -.00000135 00000-0 00000-0 0 9990
2 19772 14.9589 358.2110 0018845 115.6422 294.2098 0.99105442119291
Epoch: 2024-12-26T08:35Z
Definitive object data (Epoch: 2024-12-26T08:35:47.685Z)
Latitude | 11.36248° |
Longitude | -177.41016° |
Altitude | 36,082.578 km |
Speed | 3.065 km/s |
True Right ascension | 03h 07m 30s |
True Declination | 11° 21' 05" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -7.4074° |
Longitude | -17.01921° |
Altitude | 36,123.713 km |
Speed | 3.062 km/s |
Apparent Right ascension | 13h 22m 45s |
Apparent Declination | -13° 05' 38" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 18:43:33 |
Azimuth | 253.728° W |
Elevation | -1.043° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 36,197.808 km |
Perigee altitude | 36,037.641 km |
Semi-major axis | 42,495.862 km |
Eccentricity | 0.0018845 |
Inclination | 14.9589° |
RAAN | 358.211° |
Arg. of periapsis | 115.6422° |
True anomaly | 294.01265° |
Mean anomaly | 294.2098° |
Eccentric anomaly | 294.11125° |
Mean motion | 0.24776 °/min |
BSTAR | Unknown |
Orbital period | 1453.05 mins |
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19772 neighbors
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Other satellites on launch #6 in the year 1989 (1989-01-27 UTC)
INTELSAT 515 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. |
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271 mins | 2024-12-27 09:36:54.939Z | 271.736° WNW | 2024-12-27 12:00:54.939Z | 272.674° WNW | 11.612° | 2024-12-27 14:07:54.939Z | 269.656° W |
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