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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Edit Public Description
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
Unknown
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 25345.90501036 -.00000262 00000-0 00000+0 0 9991
2 12472 9.6954 316.8779 0005196 310.0824 65.9487 1.00234393120974Epoch: 2025-12-11T21:43Z
TLE epoch observation values (Epoch: 2025-12-11T21:43:12.895Z)
Latitude
2.67875°
Longitude
-73.93554°
Altitude
35,787.367 km
Speed
3.075 km/s
True Right ascension
22h 10m 53s
True Declination
2° 40' 34"
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
02:27:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,820.021 km
Perigee altitude
35,776.191 km
Semi-major axis
42,176.243 km
Eccentricity
0.00052
Inclination
9.6954°
RAAN
316.8779°
Arg. of periapsis
310.0824°
True anomaly
66.00309°
Mean anomaly
65.9487°
Eccentric anomaly
65.97589°
Mean motion
0.25058 °/min
Orbital period
1,436.68 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 | 2025-12-13 03:59:12.088Z | 129.135° SE | 2025-12-14 02:22:12.088Z | 129.047° SE | 34.159° | 2025-12-14 03:59:12.088Z | 129.341° SE |
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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
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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