INTELSAT 804, 25110
Orbit data source: Space-Track
INTELSAT 804, 25110 is a payload satellite owned by INTELSAT (US) in GEO that was launched on Sun, 21 Dec 1997 UTC via an ARIANE 42L 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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25110 intel report (Beta)
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Identifier
Orbit
Country
US / ITSORelated business
Manufacturer
LMT/EW
Mission
Non-operational Civil Communications
Bus & Motor
AS7000, 2X LEROS 1B
Mass
3,455 kg wet, 1,601 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Poly + 2 Pan, 10.8 m
Radar Cross Section
42.091 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 INTELSAT 804
1 25110U 97083A 26087.57781350 -.00000084 00000-0 00000+0 0 9997
2 25110 13.0709 18.2279 0009662 15.6735 167.0086 1.00262267103525Epoch: 2026-03-28T13:52Z
TLE epoch observation values (Epoch: 2026-03-28T13:52:03.086Z)
Latitude
-0.61776°
Longitude
166.87989°
Altitude
35,828.722 km
Speed
3.072 km/s
True Right ascension
13h 23m 33s
True Declination
0° 37' 02"
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
10:52:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,830.997 km
Perigee altitude
35,749.51 km
Semi-major axis
42,168.391 km
Eccentricity
0.00097
Inclination
13.0709°
RAAN
18.2279°
Arg. of periapsis
15.6735°
True anomaly
167.03346°
Mean anomaly
167.0086°
Eccentric anomaly
167.02103°
Mean motion
0.25065 °/min
Orbital period
1,436.28 mins
BSTAR
0
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Other satellites on launch #83 in the year 1997 (1997-12-21 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.INTELSAT 804 Visibility
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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. |
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| INTELSAT 804 is likely not visible in the next few days. |
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25110 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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