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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
1 day 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, 0.7 m
Radar Cross Section
2.199 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago
0 INTELSAT 2-F3
1 02717U 67026A   25199.19845262 -.00000056  00000-0  00000-0 0  9993
2 02717   3.2524  69.7977 0016673 214.4651  76.2159  1.00277012120548
Epoch: 2025-07-18T04:45Z
TLE epoch observation values (Epoch: 2025-07-18T04:45:46.306Z)
Latitude
-3.05526°
Longitude
-6.99572°
Altitude
35,768.305 km
Speed
3.076 km/s
True Right ascension
00h 02m 48s
True Declination
-3° 03' 08"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
1.22032°
Longitude
83.82265°
Altitude
35,853.278 km
Speed
3.07 km/s
Apparent Right ascension
06h 31m 53s
Apparent Declination
-4° 12' 09"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
23:34:18
Azimuth
83.922° E
Elevation
-13.719°
Doppler factor
1
Orbital elements
Apogee altitude
35,856.496 km
Perigee altitude
35,715.894 km
Semi-major axis
42,164.332 km
Eccentricity
0.00167
Inclination
3.2524°
RAAN
69.7977°
Arg. of periapsis
214.4651°
True anomaly
76.40155°
Mean anomaly
76.2159°
Eccentric anomaly
76.30871°
Mean motion
0.25068 °/min
Orbital period
1,436.08 mins
BSTAR
0
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Other satellites on launch #26 in the year 1967 (1967-03-23 UTC)
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