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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). 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.

Not visible in the next 10 days
Identifier
2717, 1967-026A
Orbit
GEO
Country
Flag of UnknownUnknown / ITSO
Related business
Manufacturer
Hughes
Mission
Non-operational spacecraft
Bus & Motor
HS-303, SVM-1
Mass
163 kg wet, ~65 kg dry
Launch date (UTC)
1967-03-23 (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: 8 hours ago

TLE from 8 hours ago
0 INTELSAT 2-F3
1  2717U 67026A   25303.75470719 -.00000019  00000-0  00000+0 0  9991
2  2717   3.5113  69.2942 0019523 212.3998  25.6386  1.00286326121594
Epoch: 2025-10-30T18:06Z
TLE epoch observation values (Epoch: 2025-10-30T18:06:46.701Z)
Latitude
-2.96902°
Longitude
-3.65603°
Altitude
35,708.566 km
Speed
3.08 km/s
True Right ascension
20h 29m 23s
True Declination
-2° 57' 58"
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
21:18:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,865.896 km
Perigee altitude
35,701.271 km
Semi-major axis
42,161.721 km
Eccentricity
0.00195
Inclination
3.5113°
RAAN
69.2942°
Arg. of periapsis
212.3998°
True anomaly
25.73561°
Mean anomaly
25.6386°
Eccentric anomaly
25.68709°
Mean motion
0.25071 °/min
Orbital period
1,435.94 mins
BSTAR
0
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Other satellites on launch #26 in the year 1967 (1967-03-23 UTC)

Documentation

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