INTELSAT 2-F1, 2514
Orbit data source: Space-Track
INTELSAT 2-F1, 2514 is a payload satellite owned by INTELSAT (US) in HEO that was launched on Wed, 26 Oct 1966 UTC via a THOR DELTA E1 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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2514 intel report (Beta)
INTELSAT 2-F1 details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 1 day ago |
| Origin | |
| Manufacturer | Hughes |
| Mission | Non-operational Civil Communications |
| Bus & Motor | HS-303, SVM-1 |
| Mass | 162 kg wet, 64 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Cyl, 1.4 m |
| Radar Cross Section | 2.199 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 INTELSAT 2-F1
1 02514U 66096A 25042.55809836 -.00000285 00000-0 00000-0 0 9992
2 02514 17.1209 148.5748 6348462 10.0741 358.1058 2.00583185 84977Epoch: 2025-02-11T13:23Z
Definitive object data (Epoch: 2025-02-11T13:23:39.698Z)
| Latitude | -0.00003° |
| Longitude | 165.80008° |
| Altitude | 3,351.321 km |
| Speed | 8.181 km/s |
| True Right ascension | 09h 54m 18s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 17.13957° |
| Longitude | -98.58662° |
| Altitude | 8,640.204 km |
| Speed | 6.171 km/s |
| Apparent Right ascension | 16h 07m 37s |
| Apparent Declination | 2° 04' 23" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 16:34:27 |
| Azimuth | 190.854° SSW |
| Elevation | 51.669° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 37,046.261 km |
| Perigee altitude | 3,320.992 km |
| Semi-major axis | 26,561.764 km |
| Eccentricity | 0.6348462 |
| Inclination | 17.1209° |
| RAAN | 148.5748° |
| Arg. of periapsis | 10.0741° |
| True anomaly | 349.07548° |
| Mean anomaly | 358.1058° |
| Eccentric anomaly | 354.82483° |
| Mean motion | 0.50137 °/min |
| BSTAR | Unknown |
| Orbital period | 718.03 mins |
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Other satellites on launch #96 in the year 1966 (1966-10-26 UTC)
| INTELSAT 2-F1, 2514 |
| DELTA 1 R/B(1), 2515 (Decayed) |
| DELTA 1 R/B(2) *, 11792 |
INTELSAT 2-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. |
|---|---|---|---|---|---|---|---|
| 624 mins | 2025-02-12 14:03:26.203Z | 190.834° SSW | 2025-02-12 14:11:26.203Z | 173.367° S | 38.727° | 2025-02-13 00:27:26.203Z | 162.961° S |
| 27 mins | 2025-02-13 13:36:26.203Z | 243.675° WSW | 2025-02-13 14:03:26.203Z | 180.637° SSW | 38.582° | 2025-02-13 14:03:26.203Z | 180.637° SSW |
Authenticating...
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