ESEO, 43792
Orbit data source: Space-Track
ESEO, 43792 is a payload satellite owned by ESA (ESA) in SSO that was launched on Mon, 03 Dec 2018 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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43792 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ESARelated business
Manufacturer
ESTEC/OHBI
Mission
Operational Civil Technology
Bus & Motor
ESEO, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.262 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 ESEO
1 43792U 18099AL 25301.62069875 .00002256 00000-0 17076-3 0 9995
2 43792 97.4288 343.6379 0013356 46.6348 313.5988 15.03211040377000Epoch: 2025-10-28T14:53Z
TLE epoch observation values (Epoch: 2025-10-28T14:53:48.371Z)
Latitude
-0.00002°
Longitude
82.98078°
Altitude
553.687 km
Speed
7.588 km/s
True Right ascension
22h 54m 33s
True Declination
0° 00' 00"
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
17:36:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.25 km
Perigee altitude
544.733 km
Semi-major axis
6,932.129 km
Eccentricity
0.00134
Inclination
97.4288°
RAAN
343.6379°
Arg. of periapsis
46.6348°
True anomaly
313.48784°
Mean anomaly
313.5988°
Eccentric anomaly
313.54333°
Mean motion
3.76048 °/min
Orbital period
95.73 mins
BSTAR
0.00017076
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Other satellites on launch #99 in the year 2018 (2018-12-03 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.ESEO 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-29 02:13:34.942Z | 119.103° SE | 2025-10-29 02:16:34.942Z | 58.026° ENE | 22.484° | 2025-10-29 02:18:34.942Z | 21.832° NNE |
| 4 mins | 2025-10-29 03:49:34.942Z | 236.5° WSW | 2025-10-29 03:50:34.942Z | 257.048° W | 20.012° | 2025-10-29 03:53:34.942Z | 312.51° NW |
| 6 mins | 2025-10-29 15:26:34.942Z | 33.824° NE | 2025-10-29 15:28:34.942Z | 81.482° E | 35.371° | 2025-10-29 15:32:34.942Z | 172.937° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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