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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
Last TLE update
9 hours 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)
1967-03-23 (58 years ago)
Launch vehicle
THOR DELTA E1
Launch site
Air Force Eastern Test Range (AFETR)
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 9 hours ago
0 INTELSAT 2-F3
1 02717U 67026A   25183.92205638 -.00000055  00000-0  00000-0 0  9993
2 02717   3.2156  69.8513 0016641 215.5230 320.2856  1.00275928120399
Epoch: 2025-07-02T22:07Z
TLE epoch observation values (Epoch: 2025-07-02T22:07:45.671Z)
Latitude
0.22947°
Longitude
-7.58098°
Altitude
35,730.708 km
Speed
3.079 km/s
True Right ascension
16h 22m 13s
True Declination
0° 13' 45"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-2.32857°
Longitude
130.4143°
Altitude
35,795.175 km
Speed
3.074 km/s
Apparent Right ascension
02h 00m 04s
Apparent Declination
-7° 38' 39"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
19:02:38
Azimuth
86.681° E
Elevation
-15.894°
Doppler factor
1
Orbital elements
Apogee altitude
35,856.665 km
Perigee altitude
35,716.333 km
Semi-major axis
42,164.636 km
Eccentricity
0.00166
Inclination
3.2156°
RAAN
69.8513°
Arg. of periapsis
215.523°
True anomaly
Unknown
Mean anomaly
320.2856°
Eccentric anomaly
Unknown
Mean motion
0.25068 °/min
Orbital period
1,436.09 mins
BSTAR
0
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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 Visibility

Observer location: undefined°, undefined°

INTELSAT 2-F3 is likely not visible in the next few days
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