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 | 6 days 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 6 days ago
0 INTELSAT 2-F1
1 02514U 66096A 25030.59377541 -.00000143 00000-0 00000-0 0 9999
2 02514 17.1059 150.8019 6349888 5.9148 358.7994 2.00581723 84739Epoch: 2025-01-30T14:15Z
Definitive object data (Epoch: 2025-01-30T14:15:02.195Z)
| Latitude | -0.00023° |
| Longitude | 166.9485° |
| Altitude | 3,315.12 km |
| Speed | 8.199 km/s |
| True Right ascension | 10h 03m 06s |
| True Declination | 0° 00' 01" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -0.44183° |
| Longitude | -12.75816° |
| Altitude | 36,572.876 km |
| Speed | 1.885 km/s |
| Apparent Right ascension | 22h 11m 05s |
| Apparent Declination | -6° 34' 22" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 21:10:40 |
| Azimuth | 159.789° S |
| Elevation | 41.465° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 37,050.264 km |
| Perigee altitude | 3,317.252 km |
| Semi-major axis | 26,561.895 km |
| Eccentricity | 0.6349888 |
| Inclination | 17.1059° |
| RAAN | 150.8019° |
| Arg. of periapsis | 5.9148° |
| True anomaly | 353.05185° |
| Mean anomaly | 358.7994° |
| Eccentric anomaly | 356.71392° |
| Mean motion | 0.50137 °/min |
| BSTAR | Unknown |
| Orbital period | 718.04 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. |
|---|---|---|---|---|---|---|---|
| 351 mins | 2025-02-05 19:06:24.838Z | 159.796° S | 2025-02-05 19:06:24.838Z | 159.796° S | 33.504° | 2025-02-06 00:57:24.838Z | 164.113° S |
| 300 mins | 2025-02-06 14:06:24.838Z | 243.532° WSW | 2025-02-06 14:39:24.838Z | 171.626° S | 38.873° | 2025-02-06 19:06:24.838Z | 160.273° S |
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