GOES 14, 35491
Orbit data source: Space-Track
GOES 14, 35491 is a payload satellite owned by NOAA (US) in GEO that was launched on Sat, 27 Jun 2009 UTC via a DELTA 4M+(4,2) 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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35491 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Boeing/ES
Mission
On reserve Civil Weather
Bus & Motor
HS-601, R-4D?
Mass
3,209 kg wet, 1,543 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan + 1 Ant, 15.0 m
Radar Cross Section
14.281 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 GOES 14
1 35491U 09033A 26139.82698780 -.00000166 00000-0 00000-0 0 9990
2 35491 1.6187 83.3539 0001609 337.4182 272.2522 1.00117069 6308Epoch: 2026-05-19T19:50Z
TLE epoch observation values (Epoch: 2026-05-19T19:50:51.745Z)
Latitude
-1.51054°
Longitude
157.78922°
Altitude
35,829.46 km
Speed
3.073 km/s
True Right ascension
22h 12m 00s
True Declination
-1° 30' 32"
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
12:43:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,837.883 km
Perigee altitude
35,824.3 km
Semi-major axis
42,209.228 km
Eccentricity
0.00016
Inclination
1.6187°
RAAN
83.3539°
Arg. of periapsis
337.4182°
True anomaly
272.23378°
Mean anomaly
272.2522°
Eccentric anomaly
272.24299°
Mean motion
0.25028 °/min
Orbital period
1,438.37 mins
BSTAR
0
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Other satellites on launch #33 in the year 2009 (2009-06-27 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.GOES 14 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. |
|---|---|---|---|---|---|---|---|
| GOES 14 is likely not visible in the next few days. |
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35491 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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