GOES 5, 12472
Orbit data source: Space-Track
GOES 5, 12472 is a payload satellite owned by NOAA (US) in GEO that was launched on Fri, 22 May 1981 UTC via a DELTA 3914 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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12472 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Hughes
Mission
Non-operational spacecraft
Bus & Motor
HS-371, STAR 27 TE-
Mass
836 kg wet, ~295 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
CYL + ANT, 2.2 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GOES 5
1 12472U 81049A 26251.26779502 .00000043 00000-0 00000+0 0 9998
2 12472 9.2158 315.1766 0003724 309.9207 47.6588 1.00224759123675Epoch: 2026-09-08T06:25Z
TLE epoch observation values (Epoch: 2026-09-08T06:25:37.489Z)
Latitude
-0.38556°
Longitude
-130.9068°
Altitude
35,788.789 km
Speed
3.075 km/s
True Right ascension
20h 51m 20s
True Declination
0° 23' 07"
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
00:30:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,816.521 km
Perigee altitude
35,785.106 km
Semi-major axis
42,178.95 km
Eccentricity
0.00037
Inclination
9.2158°
RAAN
315.1766°
Arg. of periapsis
309.9207°
True anomaly
47.69035°
Mean anomaly
47.6588°
Eccentric anomaly
47.67458°
Mean motion
0.25055 °/min
Orbital period
1,436.82 mins
BSTAR
0
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Other satellites on launch #49 in the year 1981 (1981-05-22 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 5 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 | 2026-09-09 08:17:39.752Z | 220.418° SW | 2026-09-09 12:43:39.752Z | 224.095° SW | 45.468° | 2026-09-10 08:17:39.752Z | 220.726° SW |
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12472 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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