INTELSAT 10 (PAS 10), 26766
Orbit data source: Space-Track
INTELSAT 10 (PAS 10), 26766 is a payload satellite owned by Panamsat (US) in GEO that was launched on Tue, 15 May 2001 UTC via a PROTON-K/DM-2M launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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26766 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Boeing/ES
Mission
Operational Commercial Communications
Bus & Motor
HS-601HP, R-4D-11-300
Mass
3,772 kg wet, ~2,000 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: 17 hours ago
TLE from 17 hours ago
0 INTELSAT 10 (PAS 10)
1 26766U 01019A 25258.21781128 -.00000278 00000-0 00000-0 0 9998
2 26766 8.4132 62.0403 0003421 182.4584 347.9677 0.99080288 42850Epoch: 2025-09-15T05:13Z
TLE epoch observation values (Epoch: 2025-09-15T05:13:38.894Z)
Latitude
1.41202°
Longitude
159.71529°
Altitude
36,109.128 km
Speed
3.064 km/s
True Right ascension
15h 30m 12s
True Declination
1° 24' 38"
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
15:18:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,139.527 km
Perigee altitude
36,110.446 km
Semi-major axis
42,503.124 km
Eccentricity
0.00034
Inclination
8.4132°
RAAN
62.0403°
Arg. of periapsis
182.4584°
True anomaly
347.95952°
Mean anomaly
347.9677°
Eccentric anomaly
347.96361°
Mean motion
0.24769 °/min
Orbital period
1,453.42 mins
BSTAR
0
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Other satellites on launch #19 in the year 2001 (2001-05-15 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 10 (PAS 10) 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 10 (PAS 10) is likely not visible in the next few days. |
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26766 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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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 ascending order |
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