DOORY-SAT, 58500
Orbit data source: Space-Track
DOORY-SAT, 58500 is a payload satellite owned by Hanwha (KR) in LEO that was launched on Mon, 04 Dec 2023 UTC via an ADD TV2 launch vehicle from the Jeju Sea Launch Area (JJSLA). 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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58500 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / SKORRelated business
Manufacturer
Hanwha
Mission
Operational Commercial Radar Imaging
Bus & Motor
S-STEP, Unknown motor
Mass
80 kg wet, 80 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
2.400 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 DOORY-SAT
1 58500U 23188A 25293.63124028 .00003254 00000-0 45525-3 0 9995
2 58500 46.9831 26.9296 0008952 330.5976 29.4413 14.79660815101509Epoch: 2025-10-20T15:08Z
TLE epoch observation values (Epoch: 2025-10-20T15:08:59.160Z)
Latitude
-0.00004°
Longitude
130.35229°
Altitude
625.149 km
Speed
7.55 km/s
True Right ascension
01h 47m 43s
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
17:50:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
637.92 km
Perigee altitude
625.369 km
Semi-major axis
7,009.781 km
Eccentricity
0.0009
Inclination
46.9831°
RAAN
26.9296°
Arg. of periapsis
330.5976°
True anomaly
29.49177°
Mean anomaly
29.4413°
Eccentric anomaly
29.46653°
Mean motion
3.69817 °/min
Orbital period
97.35 mins
BSTAR
0.00045525
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Other satellites on launch #188 in the year 2023 (2023-12-04 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.DOORY-SAT 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-21 09:09:31.889Z | 214.723° SW | 2025-10-21 09:13:31.889Z | 124.746° SE | 36.102° | 2025-10-21 09:16:31.889Z | 74.106° E |
| 7 mins | 2025-10-21 10:52:31.889Z | 276.617° WNW | 2025-10-21 10:55:31.889Z | 1.749° NNE | 36.309° | 2025-10-21 10:59:31.889Z | 57.409° ENE |
| 7 mins | 2025-10-21 12:34:31.889Z | 303.181° NW | 2025-10-21 12:37:31.889Z | 356.823° N | 28.938° | 2025-10-21 12:41:31.889Z | 64.871° ENE |
| 7 mins | 2025-10-21 14:17:31.889Z | 309.806° NW | 2025-10-21 14:20:31.889Z | 37.559° NE | 39.501° | 2025-10-21 14:24:31.889Z | 99.691° ESE |
| 6 mins | 2025-10-21 15:59:31.889Z | 274.564° WNW | 2025-10-21 16:02:31.889Z | 205.015° SW | 31.432° | 2025-10-21 16:05:31.889Z | 155.254° SSE |
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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