ICO G-1, 32763
Orbit data source: Space-Track
ICO G-1, 32763 is a payload satellite owned by ICO North America (US) in GEO that was launched on Mon, 14 Apr 2008 UTC via an ATLAS V 421 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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32763 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SS/Loral
Mission
Operational Commercial Communications
Bus & Motor
SSL-1300, R-4D-15-300
Mass
6,600 kg wet, ~3,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 15.0 m
Radar Cross Section
50.806 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ICO G-1
1 32763U 08016A 25291.89195894 -.00000173 00000-0 00000-0 0 9990
2 32763 5.5004 36.6987 0002329 159.8146 59.3925 1.00271709 64129Epoch: 2025-10-18T21:24Z
TLE epoch observation values (Epoch: 2025-10-18T21:24:25.252Z)
Latitude
-3.46779°
Longitude
-92.93995°
Altitude
35,781.607 km
Speed
3.075 km/s
True Right ascension
17h 03m 07s
True Declination
-3° 27' 51"
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
03:17:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,797.493 km
Perigee altitude
35,777.852 km
Semi-major axis
42,165.809 km
Eccentricity
0.00023
Inclination
5.5004°
RAAN
36.6987°
Arg. of periapsis
159.8146°
True anomaly
59.41547°
Mean anomaly
59.3925°
Eccentric anomaly
59.40399°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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Other satellites on launch #16 in the year 2008 (2008-04-14 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.ICO G-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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2025-10-19 08:25:39.063Z | 160.538° S | 2025-10-19 12:45:39.063Z | 159.008° S | 36.639° | 2025-10-20 08:25:39.063Z | 160.513° S |
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32763 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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