STAR ONE C2, 32768
Orbit data source: Space-Track
STAR ONE C2, 32768 is a payload satellite owned by Star One (BR) in GEO that was launched on Fri, 18 Apr 2008 UTC via an ARIANE 5ECA launch vehicle from the French Guiana (FRGUI). 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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32768 intel report (Beta)
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Identifier
Orbit
Country
BR / BRAZRelated business
Manufacturer
Thales Alenia
Mission
Operational Commercial Communications
Bus & Motor
SPACEBUS 3000B3, S400
Mass
4,100 kg wet, 1,750 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 11.2 m
Radar Cross Section
25.359 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 STAR ONE C2
1 32768U 08018B 26094.87643987 -.00000275 00000-0 00000-0 0 9991
2 32768 1.0537 83.0721 0003094 307.0841 53.5444 1.00270759 65911Epoch: 2026-04-04T21:02Z
TLE epoch observation values (Epoch: 2026-04-04T21:02:04.404Z)
Latitude
-0.00584°
Longitude
-64.97318°
Altitude
35,778.615 km
Speed
3.075 km/s
True Right ascension
05h 34m 56s
True Declination
0° 00' 21"
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
12:05:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,800.999 km
Perigee altitude
35,774.906 km
Semi-major axis
42,166.089 km
Eccentricity
0.00031
Inclination
1.0537°
RAAN
83.0721°
Arg. of periapsis
307.0841°
True anomaly
53.57292°
Mean anomaly
53.5444°
Eccentric anomaly
53.55866°
Mean motion
0.25067 °/min
Orbital period
1,436.16 mins
BSTAR
0
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Other satellites on launch #18 in the year 2008 (2008-04-18 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.STAR ONE C2 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 | 2026-04-05 06:11:13.888Z | 126.747° SE | 2026-04-06 03:09:13.888Z | 126.472° SE | 25.967° | 2026-04-06 06:11:13.888Z | 126.763° SE |
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32768 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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