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.
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2717 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ITSORelated business
Manufacturer
Hughes
Mission
Non-operational spacecraft
Bus & Motor
HS-303, SVM-1
Mass
163 kg wet, ~65 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 INTELSAT 2-F3
1 2717U 67026A 25363.75313522 .00000019 00000-0 00000+0 0 9994
2 2717 3.6619 69.0315 0020597 218.1116 82.8083 1.00295319122195Epoch: 2025-12-29T18:04Z
TLE epoch observation values (Epoch: 2025-12-29T18:04:30.883Z)
Latitude
-3.13641°
Longitude
0.66172°
Altitude
35,769.412 km
Speed
3.076 km/s
True Right ascension
00h 40m 56s
True Declination
-3° 07' 60"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
05:21:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,867.898 km
Perigee altitude
35,694.228 km
Semi-major axis
42,159.2 km
Eccentricity
0.00206
Inclination
3.6619°
RAAN
69.0315°
Arg. of periapsis
218.1116°
True anomaly
83.04254°
Mean anomaly
82.8083°
Eccentric anomaly
82.92541°
Mean motion
0.25073 °/min
Orbital period
1,435.81 mins
BSTAR
0
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Other satellites on launch #26 in the year 1967 (1967-03-23 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.INTELSAT 2-F3 Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| INTELSAT 2-F3 is likely not visible in the next few days. |
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2717 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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