OBJECT D, 59813 (Decayed)
Orbit data source: Space-Track
OBJECT D, 59813 was a Chinese satellite in SSO that was launched on Tue, 21 May 2024 UTC via a KUAIZHOU-11 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.
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59813 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Decayed Commercial Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.126 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 OBJECT D
1 59813U 24095D 26073.43859705 .02028235 37939-2 21941-2 0 9999
2 59813 97.5254 178.3175 0009077 281.6240 78.4024 16.10841119101658Epoch: 2026-03-14T10:31Z
TLE epoch observation values (Epoch: 2026-03-14T10:31:34.785Z)
Latitude
-0.00005°
Longitude
-151.6372°
Altitude
246.542 km
Speed
7.76 km/s
True Right ascension
11h 53m 16s
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
23:50:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
247.397 km
Perigee altitude
235.38 km
Semi-major axis
6,619.525 km
Eccentricity
0.00091
Inclination
97.5254°
RAAN
178.3175°
Arg. of periapsis
281.624°
True anomaly
78.50431°
Mean anomaly
78.4024°
Eccentric anomaly
78.45335°
Mean motion
4.02998 °/min
Orbital period
89.33 mins
BSTAR
0.0021941
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Other satellites on launch #95 in the year 2024 (2024-05-21 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.OBJECT D 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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| This satellite is decayed. |
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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