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)
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INTELSAT 1-F1 details
| Identifier | |
| Orbit | GEO |
| Last TLE update | 2 days 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 2 days ago
0 INTELSAT 1-F1
1 01317U 65028A 24295.27533017 -.00000194 00000-0 00000-0 0 9998
2 01317 5.6788 69.6041 0008140 129.8067 199.2730 1.00361449121115Epoch: 2024-10-21T06:36Z
Definitive object data (Epoch: 2024-10-21T06:36:28.526Z)
| Latitude | -2.90905° |
| Longitude | -90.57027° |
| Altitude | 35,793.958 km |
| Speed | 3.073 km/s |
| True Right ascension | 02h 35m 00s |
| True Declination | -2° 54' 22" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 2.63032° |
| Longitude | 92.67767° |
| Altitude | 35,728.896 km |
| Speed | 3.078 km/s |
| Apparent Right ascension | 14h 55m 49s |
| Apparent Declination | -3° 16' 46" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 13:47:36 |
| Azimuth | 155.958° SSE |
| Elevation | 44.055° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 35,796.836 km |
| Perigee | 35,728.231 km |
| Semi-major axis | 42,140.67 km |
| Eccentricity | 0.000814 |
| Inclination | 5.6788° |
| RAAN | 69.6041° |
| Arg. of periapsis | 129.8067° |
| True anomaly | 199.24224° |
| Mean anomaly | 199.273° |
| Eccentric anomaly | 199.25762° |
| Mean motion | 0.25089 °/min |
| BSTAR | Unknown |
| Period | 1434.87 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: 39.9160978°, -105.1181434
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 | 2024-10-22 18:41:20.639Z | 155.967° SSE | 2024-10-23 14:24:20.639Z | 154.309° SSE | 36.292° | 2024-10-23 18:41:20.639Z | 155.548° SSE |