EUTE 36D, 59346
Orbit data source: Space-Track
EUTE 36D, 59346 is a payload satellite owned by EutelsatSA (FR) in GEO that was launched on Sat, 30 Mar 2024 UTC via an FALCON 9 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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59346 intel report (Beta)
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Identifier
Orbit
Country
FR / EUTERelated business
Manufacturer
ADST/ADSUK
Mission
Operational Commercial Communications
Bus & Motor
EUROSTAR NEO, PPS-5000
Mass
5,000 kg wet, ~5,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 20.0 m
Radar Cross Section
58.239 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 EUTE 36D
1 59346U 24059A 26094.86294936 .00000156 00000-0 00000-0 0 9997
2 59346 0.0187 172.2170 0000635 276.1683 91.3166 1.00271992 7411Epoch: 2026-04-04T20:42Z
TLE epoch observation values (Epoch: 2026-04-04T20:42:38.824Z)
Latitude
-0.00549°
Longitude
35.87756°
Altitude
35,786.098 km
Speed
3.075 km/s
True Right ascension
11h 58m 51s
True Declination
0° 00' 20"
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
16:12:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,790.285 km
Perigee altitude
35,784.93 km
Semi-major axis
42,165.744 km
Eccentricity
0.00006
Inclination
0.0187°
RAAN
172.217°
Arg. of periapsis
276.1683°
True anomaly
91.32387°
Mean anomaly
91.3166°
Eccentric anomaly
91.32024°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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Other satellites on launch #59 in the year 2024 (2024-03-30 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.EUTE 36D 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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| EUTE 36D is likely not visible in the next few days. |
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59346 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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