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, 13.5 m
Radar Cross Section
38.593 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 GALAXY 28 (IA 8)
1 28702U 05022A 25306.48621059 -.00000173 00000-0 00000+0 0 9990
2 28702 2.7114 81.7519 0002272 169.3335 237.2939 1.00272793 49706Epoch: 2025-11-02T11:40Z
TLE epoch observation values (Epoch: 2025-11-02T11:40:08.594Z)
Latitude
1.9519°
Longitude
-88.75046°
Altitude
35,790.732 km
Speed
3.074 km/s
True Right ascension
08h 33m 08s
True Declination
1° 56' 60"
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
23:24:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,796.959 km
Perigee altitude
35,777.799 km
Semi-major axis
42,165.516 km
Eccentricity
0.00023
Inclination
2.7114°
RAAN
81.7519°
Arg. of periapsis
169.3335°
True anomaly
237.272°
Mean anomaly
237.2939°
Eccentric anomaly
237.28295°
Mean motion
0.25067 °/min
Orbital period
1,436.14 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 | 2025-11-04 03:29:58.474Z | 156.431° SSE | 2025-11-04 14:29:58.474Z | 154.007° SSE | 34.612° | 2025-11-05 03:29:58.474Z | 156.42° 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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