GOES 17, 43226
Orbit data source: Space-Track
GOES 17, 43226 is a payload satellite owned by NOAA (US) in GEO that was launched on Thu, 01 Mar 2018 UTC via an ATLAS V 541 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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43226 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
LMCSS
Mission
On reserve Civil Weather
Bus & Motor
A2100, LEROS-1C
Mass
5,192 kg wet, 2,857 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan + 1 Ant, 20.0 m
Radar Cross Section
38.538 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 GOES 17
1 43226U 18022A 25306.48609963 -.00000170 00000-0 00000+0 0 9999
2 43226 0.3500 89.9891 0003156 167.6592 229.8844 1.00270434 28156Epoch: 2025-11-02T11:39Z
TLE epoch observation values (Epoch: 2025-11-02T11:39:59.008Z)
Latitude
0.1922°
Longitude
-89.53172°
Altitude
35,794.981 km
Speed
3.074 km/s
True Right ascension
08h 29m 51s
True Declination
0° 11' 31"
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
12:03:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,801.352 km
Perigee altitude
35,774.736 km
Semi-major axis
42,166.181 km
Eccentricity
0.00032
Inclination
0.35°
RAAN
89.9891°
Arg. of periapsis
167.6592°
True anomaly
229.85675°
Mean anomaly
229.8844°
Eccentric anomaly
229.87057°
Mean motion
0.25067 °/min
Orbital period
1,436.17 mins
BSTAR
0
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Other satellites on launch #22 in the year 2018 (2018-03-01 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 17 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 | 2025-11-02 16:15:20.178Z | 156.356° SSE | 2025-11-03 15:25:20.178Z | 156.363° SSE | 33.502° | 2025-11-03 16:15:20.178Z | 156.364° SSE |
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43226 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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