JUPITER 3 (ECHOSTAR 24), 57479
Orbit data source: Space-Track
JUPITER 3 (ECHOSTAR 24), 57479 is an American payload satellite in GEO that was launched on Sat, 29 Jul 2023 UTC via an FALCON HEAVY 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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57479 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Maxar Space Sol
Mission
Operational Commercial Communications
Bus & Motor
SSL-1300, SPT-100
Mass
9,200 kg wet, ~5,817 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 19.4 m
Radar Cross Section
56.895 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 JUPITER 3 (ECHOSTAR 24)
1 57479U 23108A 25297.17323410 -.00000138 00000-0 00000-0 0 9995
2 57479 0.0130 248.8456 0001328 327.5543 143.6262 1.00271478 8280Epoch: 2025-10-24T04:09Z
TLE epoch observation values (Epoch: 2025-10-24T04:09:27.426Z)
Latitude
0.03382°
Longitude
-95.18623°
Altitude
35,790.697 km
Speed
3.074 km/s
True Right ascension
23h 59m 59s
True Declination
0° 02' 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
17:35:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,793.351 km
Perigee altitude
35,782.152 km
Semi-major axis
42,165.888 km
Eccentricity
0.00013
Inclination
0.013°
RAAN
248.8456°
Arg. of periapsis
327.5543°
True anomaly
143.63522°
Mean anomaly
143.6262°
Eccentric anomaly
143.63071°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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Other satellites on launch #108 in the year 2023 (2023-07-29 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.JUPITER 3 (ECHOSTAR 24) 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 | 2025-10-25 22:17:36.590Z | 164.725° S | 2025-10-26 04:17:36.590Z | 164.728° S | 34.159° | 2025-10-26 22:17:36.590Z | 164.728° S |
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57479 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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