INTELSAT 2-F4, 2969
Orbit data source: Space-Track
INTELSAT 2-F4, 2969 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Thu, 28 Sep 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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2969 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 S/N 3
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: 6 hours ago
TLE from 6 hours ago
0 INTELSAT 2-F4
1 2969U 67094A 25312.18024937 .00000136 00000-0 00000+0 0 9998
2 2969 3.5123 76.4766 0013739 142.8700 100.3303 1.00337790113097Epoch: 2025-11-08T04:19Z
TLE epoch observation values (Epoch: 2025-11-08T04:19:33.545Z)
Latitude
-3.12986°
Longitude
-152.7381°
Altitude
35,778.439 km
Speed
3.075 km/s
True Right ascension
21h 19m 03s
True Declination
-3° 07' 36"
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
06:46:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,827.073 km
Perigee altitude
35,711.26 km
Semi-major axis
42,147.303 km
Eccentricity
0.00137
Inclination
3.5123°
RAAN
76.4766°
Arg. of periapsis
142.87°
True anomaly
100.48514°
Mean anomaly
100.3303°
Eccentric anomaly
100.40772°
Mean motion
0.25084 °/min
Orbital period
1,435.21 mins
BSTAR
0
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Other satellites on launch #94 in the year 1967 (1967-09-28 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-F4 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-11-08 10:35:17.729Z | 238.693° WSW | 2025-11-08 18:24:17.729Z | 242.505° WSW | 23.542° | 2025-11-09 10:35:17.729Z | 238.536° WSW |
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2969 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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