INTELSAT 1-F1, 1317
Orbit data source: Space-Track
INTELSAT 1-F1, 1317 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Tue, 06 Apr 1965 UTC via a THOR DELTA D 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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1317 intel report (Beta)
INTELSAT 1-F1 details
Identifier | |
Orbit | GEO |
Last TLE update | 9 hours ago |
Origin | |
Manufacturer | Hughes |
Mission | Non-operational Civil Communications |
Bus & Motor | HS-303A, STARFINDER |
Mass | 68 kg wet, 30 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Cyl, 0.72 m |
Radar Cross Section | 0.543 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 9 hours ago
0 INTELSAT 1-F1
1 1317U 65028A 24361.08653786 -.00000246 00000-0 00000+0 0 9994
2 1317 5.8428 69.0368 0006771 146.9083 198.9119 1.00343000121783
Epoch: 2024-12-26T02:04Z
Definitive object data (Epoch: 2024-12-26T02:04:36.871Z)
Latitude | -1.41839° |
Longitude | -71.32567° |
Altitude | 35,793.343 km |
Speed | 3.073 km/s |
True Right ascension | 03h 39m 35s |
True Declination | -1° 25' 01" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 5.23958° |
Longitude | 59.31803° |
Altitude | 35,741.183 km |
Speed | 3.077 km/s |
Apparent Right ascension | 12h 38m 40s |
Apparent Declination | 0° 20' 40" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 10:06:28 |
Azimuth | 129.6° SE |
Elevation | 36.877° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 35,796.234 km |
Perigee altitude | 35,739.16 km |
Semi-major axis | 42,145.834 km |
Eccentricity | 0.0006771 |
Inclination | 5.8428° |
RAAN | 69.0368° |
Arg. of periapsis | 146.9083° |
True anomaly | 198.88677° |
Mean anomaly | 198.9119° |
Eccentric anomaly | 198.89933° |
Mean motion | 0.25085 °/min |
BSTAR | Unknown |
Orbital period | 1435.13 mins |
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1317 neighbors
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Other satellites on launch #28 in the year 1965 (1965-04-06 UTC)
INTELSAT 1-F1, 1317 |
DELTA 1 R/B(2), 1318 |
INTELSAT 1-F1 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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1440 mins | 2024-12-26 10:45:14.594Z | 129.616° SE | 2024-12-27 08:44:14.594Z | 129.023° SE | 31.255° | 2024-12-27 10:45:14.594Z | 129.372° SE |
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