INTELSAT 2-F3, 2717
Orbit data source: Space-Track
INTELSAT 2-F3, 2717 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Thu, 23 Mar 1967 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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2717 intel report (Beta)
INTELSAT 2-F3 details
Identifier | |
Orbit | GEO |
Last TLE update | 2 days ago |
Origin | |
Manufacturer | Hughes |
Mission | Non-operational Civil Communications |
Bus & Motor | HS-303, SVM-1 |
Mass | 163 kg wet, ~65 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 2 days ago
0 INTELSAT 2-F3
1 02717U 67026A 25045.82637247 -.00000066 00000-0 00000-0 0 9996
2 02717 2.8743 70.1487 0019608 216.0764 148.7666 1.00267831119018
Epoch: 2025-02-14T19:49Z
Definitive object data (Epoch: 2025-02-14T19:49:58.581Z)
Latitude | 0.23124° |
Longitude | -7.44498° |
Altitude | 35,857.763 km |
Speed | 3.07 km/s |
True Right ascension | 05h 00m 31s |
True Declination | 0° 13' 52" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | 2.72413° |
Longitude | 58.29208° |
Altitude | 35,855.026 km |
Speed | 3.07 km/s |
Apparent Right ascension | 09h 49m 22s |
Apparent Declination | -2° 44' 41" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 02:53:58 |
Azimuth | 83.139° E |
Elevation | -12.363° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 35,871.451 km |
Perigee altitude | 35,706.089 km |
Semi-major axis | 42,166.907 km |
Eccentricity | 0.0019608 |
Inclination | 2.8743° |
RAAN | 70.1487° |
Arg. of periapsis | 216.0764° |
True anomaly | 148.88286° |
Mean anomaly | 148.7666° |
Eccentric anomaly | 148.82476° |
Mean motion | 0.25066 °/min |
BSTAR | Unknown |
Orbital period | 1436.21 mins |
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2717 neighbors
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Other satellites on launch #26 in the year 1967 (1967-03-23 UTC)
INTELSAT 2-F3, 2717 |
DELTA 1 R/B(1), 2719 (Decayed) |
DELTA 1 R/B(2), 11984 |
INTELSAT 2-F3 Visibility forecast
Observer location: undefined°, undefined
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