SBS 1, 12065
Orbit data source: Space-Track
SBS 1, 12065 is a payload satellite owned by SBS (US) in GEO that was launched on Sat, 15 Nov 1980 UTC via a DELTA 3910/PAM 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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12065 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Hughes
Mission
Spacecraft
Bus & Motor
HS-376, TE-M-700-5
Mass
~1,064 kg wet, 424 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: 2 days ago
TLE from 2 days ago
0 SBS 1
1 12065U 80091A 25312.71409455 .00000078 00000-0 00000+0 0 9994
2 12065 10.3764 319.2450 0008346 211.3111 337.0666 0.99824511 44279Epoch: 2025-11-08T17:08Z
TLE epoch observation values (Epoch: 2025-11-08T17:08:17.769Z)
Latitude
-1.51063°
Longitude
-157.78562°
Altitude
35,879.822 km
Speed
3.072 km/s
True Right ascension
09h 49m 42s
True Declination
-1° 30' 33"
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
03:04:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,948.763 km
Perigee altitude
35,878.17 km
Semi-major axis
42,291.604 km
Eccentricity
0.00083
Inclination
10.3764°
RAAN
319.245°
Arg. of periapsis
211.3111°
True anomaly
337.0293°
Mean anomaly
337.0666°
Eccentric anomaly
337.04795°
Mean motion
0.24955 °/min
Orbital period
1,442.58 mins
BSTAR
0
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Other satellites on launch #91 in the year 1980 (1980-11-15 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.SBS 1 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. |
|---|---|---|---|---|---|---|---|
| 832 mins | 2025-11-10 06:45:54.411Z | 250.574° W | 2025-11-10 10:55:54.411Z | 254.708° W | 23.039° | 2025-11-10 20:37:54.411Z | 240.217° WSW |
| 388 mins | 2025-11-11 00:17:54.411Z | 239.419° WSW | 2025-11-11 06:45:54.411Z | 251.741° W | 19.103° | 2025-11-11 06:45:54.411Z | 251.741° W |
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12065 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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