AMOS 4, 39237
Orbit data source: Space-Track
AMOS 4, 39237 is a payload satellite owned by IAI Spacecom (IL) in GEO that was launched on Sat, 31 Aug 2013 UTC via a ZENIT-3SLB launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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39237 intel report (Beta)
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Identifier
Orbit
Country
IL / ISRARelated business
Manufacturer
IAI
Mission
Operational Civil Communications
Bus & Motor
AMOS-HP, S400
Mass
4,260 kg wet, ~2,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 8.7 m
Radar Cross Section
30.054 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 AMOS 4
1 39237U 13045A 26135.11606944 .00000020 00000-0 00000-0 0 9997
2 39237 0.0507 101.0883 0002873 295.1256 303.4220 1.00272474 46628Epoch: 2026-05-15T02:47Z
TLE epoch observation values (Epoch: 2026-05-15T02:47:08.399Z)
Latitude
-0.01422°
Longitude
64.9553°
Altitude
35,779.222 km
Speed
3.075 km/s
True Right ascension
22h 38m 22s
True Declination
0° 00' 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
23:05:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,799.586 km
Perigee altitude
35,775.358 km
Semi-major axis
42,165.609 km
Eccentricity
0.00029
Inclination
0.0507°
RAAN
101.0883°
Arg. of periapsis
295.1256°
True anomaly
303.39452°
Mean anomaly
303.422°
Eccentric anomaly
303.40826°
Mean motion
0.25067 °/min
Orbital period
1,436.14 mins
BSTAR
0
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Other satellites on launch #45 in the year 2013 (2013-08-31 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.AMOS 4 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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| AMOS 4 is likely not visible in the next few days. |
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39237 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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