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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). Payload-class satellites include a variety of spacecraft 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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Identifier
1317, 1965-028A
Orbit
GEO
Country
Flag of USUS / ITSO
Related business
Manufacturer
Hughes
Mission
Non-operational spacecraft
Bus & Motor
HS-303A, STARFINDER
Mass
68 kg wet, 30 kg dry
Launch date (UTC)
1965-04-06 (61 years ago)
Launch vehicle
THOR DELTA D
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 6 days ago

TLE from 6 days ago
0 INTELSAT 1-F1
1 01317U 65028A   26073.29688767 -.00000153  00000-0  00000-0 0  9994
2 01317   6.9264  64.6927 0005500 165.4151 315.9277  1.00181179126223
Epoch: 2026-03-14T07:07Z
TLE epoch observation values (Epoch: 2026-03-14T07:07:31.094Z)
Latitude
5.92505°
Longitude
-92.61095°
Altitude
35,794.282 km
Speed
3.075 km/s
True Right ascension
12h 24m 45s
True Declination
5° 55' 09"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:02:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,836.266 km
Perigee altitude
35,789.856 km
Semi-major axis
42,191.198 km
Eccentricity
0.00055
Inclination
6.9264°
RAAN
64.6927°
Arg. of periapsis
165.4151°
True anomaly
315.88384°
Mean anomaly
315.9277°
Eccentric anomaly
315.90577°
Mean motion
0.25044 °/min
Orbital period
1,437.45 mins
BSTAR
0
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Other satellites on launch #28 in the year 1965 (1965-04-06 UTC)

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