GALAXY 28 (IA 8), 28702
Orbit data source: Space-Track
GALAXY 28 (IA 8), 28702 is a payload satellite owned by Intelsat Ltd (US) (US) in GEO that was launched on Thu, 23 Jun 2005 UTC via a ZENIT-3SL launch vehicle from the Sea Launch (SEAL). 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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28702 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ITSORelated business
Manufacturer
SS/Loral
Mission
Operational Commercial Communications
Bus & Motor
SSL-1300, R-4D-11-164
Mass
5,493 kg wet, ~3,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.3 m
Radar Cross Section
38.593 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 GALAXY 28 (IA 8)
1 28702U 05022A 25261.15808508 -.00000206 00000-0 00000-0 0 9998
2 28702 2.5933 82.3281 0001909 91.9270 151.2830 1.00271832 49258Epoch: 2025-09-18T03:47Z
TLE epoch observation values (Epoch: 2025-09-18T03:47:38.55Z)
Latitude
-2.3093°
Longitude
-88.71141°
Altitude
35,793.505 km
Speed
3.074 km/s
True Right ascension
21h 42m 05s
True Declination
-2° 18' 25"
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
05:36:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,795.698 km
Perigee altitude
35,779.6 km
Semi-major axis
42,165.786 km
Eccentricity
0.00019
Inclination
2.5933°
RAAN
82.3281°
Arg. of periapsis
91.927°
True anomaly
151.29351°
Mean anomaly
151.283°
Eccentric anomaly
151.28825°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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Other satellites on launch #22 in the year 2005 (2005-06-23 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.GALAXY 28 (IA 8) 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 | 2025-09-18 12:46:16.538Z | 155.001° SSE | 2025-09-18 17:38:16.538Z | 154.034° SSE | 34.56° | 2025-09-19 12:46:16.538Z | 154.985° SSE |
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28702 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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