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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 USUS / 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: 14 hours ago

TLE from 14 hours ago
0 INTELSAT 2-F1
1 02514U 66096A   26073.96110357 -.00000310  00000-0  00000-0 0  9994
2 02514  17.6075  72.7832 6395560 148.9669 273.5827  2.00376478 92929
Epoch: 2026-03-14T23:03Z
TLE epoch observation values (Epoch: 2026-03-14T23:03:59.348Z)
Latitude
Longitude
-85.71891°
Altitude
28,292.579 km
Speed
2.828 km/s
True Right ascension
04h 51m 24s
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
17:09:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,201.335 km
Perigee altitude
3,202.481 km
Semi-major axis
26,580.045 km
Eccentricity
0.63956
Inclination
17.6075°
RAAN
72.7832°
Arg. of periapsis
148.9669°
True anomaly
211.11857°
Mean anomaly
273.5827°
Eccentric anomaly
241.40767°
Mean motion
0.50085 °/min
Orbital period
718.77 mins
BSTAR
0
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Other satellites on launch #96 in the year 1966 (1966-10-26 UTC)

Documentation

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