OBJECT A, 58917 (Decayed)
Orbit data source: Space-Track
OBJECT A, 58917 was a satellite in LEO that was launched on Sat, 03 Feb 2024 UTC via a JIELONG-3 launch vehicle from the South China Sea Launch Area (SCSLA). 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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58917 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
None
Manufacturer
Unknown
Mission
Decayed Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 3 Pan, 0.1 m
Radar Cross Section
0.135 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 OBJECT A
1 58917U 24024A 25127.30226172 .07082575 24561-5 13117-2 0 9994
2 58917 97.3220 212.8671 0014484 266.6281 93.3358 16.31958565 70562Epoch: 2025-05-07T07:15Z
TLE epoch observation values (Epoch: 2025-05-07T07:15:15.412Z)
Latitude
0.00001°
Longitude
-121.33618°
Altitude
191.092 km
Speed
7.791 km/s
True Right ascension
14h 11m 28s
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
21:32:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
193.601 km
Perigee altitude
174.591 km
Semi-major axis
6,562.233 km
Eccentricity
0.00145
Inclination
97.322°
RAAN
212.8671°
Arg. of periapsis
266.6281°
True anomaly
93.50148°
Mean anomaly
93.3358°
Eccentric anomaly
93.41864°
Mean motion
4.08287 °/min
Orbital period
88.17 mins
BSTAR
0.0013117
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Other satellites on launch #24 in the year 2024 (2024-02-03 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.OBJECT A 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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