INTELSAT 9 (PAS 9), 26451
Orbit data source: Space-Track
INTELSAT 9 (PAS 9), 26451 is a payload satellite owned by Panamsat (US) in GEO that was launched on Fri, 28 Jul 2000 UTC via a ZENIT-3SL launch vehicle from the Sea Launch (SEAL). 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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26451 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Hughes
Mission
Non-operational Commercial Communications
Bus & Motor
HS-601HP, R-4D-14-350
Mass
3,650 kg wet, ~1,900 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 13.0 m
Radar Cross Section
31.072 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 INTELSAT 9 (PAS 9)
1 26451U 00043A 26047.75194197 -.00000167 00000-0 00000+0 0 9991
2 26451 10.1133 50.3049 0004942 238.7453 123.9846 0.99407022 42913Epoch: 2026-02-16T18:02Z
TLE epoch observation values (Epoch: 2026-02-16T18:02:47.786Z)
Latitude
0.4669°
Longitude
-4.39315°
Altitude
36,041.891 km
Speed
3.065 km/s
True Right ascension
03h 32m 11s
True Declination
0° 27' 59"
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
08:36:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,052.751 km
Perigee altitude
36,010.833 km
Semi-major axis
42,409.929 km
Eccentricity
0.00049
Inclination
10.1133°
RAAN
50.3049°
Arg. of periapsis
238.7453°
True anomaly
124.03154°
Mean anomaly
123.9846°
Eccentric anomaly
124.00807°
Mean motion
0.24851 °/min
Orbital period
1,448.64 mins
BSTAR
0
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Other satellites on launch #43 in the year 2000 (2000-07-28 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 9 (PAS 9) 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 9 (PAS 9) is likely not visible in the next few days. |
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26451 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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