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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). 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
2514, 1966-096A
Orbit
HEO
Country
Flag of UnknownUnknown / ITSO
Related business
Manufacturer
Hughes
Mission
Non-operational spacecraft
Bus & Motor
HS-303, SVM-1
Mass
162 kg wet, 64 kg dry
Launch date (UTC)
1966-10-26 (59 years ago)
Launch vehicle
THOR DELTA E1
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 week ago

TLE from 1 week ago
0 INTELSAT 2-F1
1 02514U 66096A   25342.22321326 -.00000395  00000-0  00000-0 0  9994
2 02514  17.2950  91.5529 6383789 114.9742 322.0756  2.00433483 90989
Epoch: 2025-12-08T05:21Z
TLE epoch observation values (Epoch: 2025-12-08T05:21:25.625Z)
Latitude
-0.00001°
Longitude
-66.16866°
Altitude
15,246.017 km
Speed
4.676 km/s
True Right ascension
06h 05m 39s
True Declination
0° 00' 00"
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
06:39:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,161.8 km
Perigee altitude
3,231.948 km
Semi-major axis
26,575.011 km
Eccentricity
0.63838
Inclination
17.295°
RAAN
91.5529°
Arg. of periapsis
114.9742°
True anomaly
244.93709°
Mean anomaly
322.0756°
Eccentric anomaly
287.11984°
Mean motion
0.50099 °/min
Orbital period
718.57 mins
BSTAR
0
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Other satellites on launch #96 in the year 1966 (1966-10-26 UTC)

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