OBJECT E, 62056 (Decayed)
Orbit data source: Space-Track
OBJECT E, 62056 was a satellite owned by CAST IX Center (CN) in LEO that was launched on Wed, 17 Jan 2024 UTC via a CHANG ZHENG 7 launch vehicle from the Wenchang Satellite Launch Center (WSC). 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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62056 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
NANJID
Mission
Decayed Amateur Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10.1 kg wet, 10.1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 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 E
1 62056U 24013E 25073.53716870 .03010361 79304-5 61090-3 0 9994
2 62056 41.4837 215.3569 0059784 311.4335 48.1400 16.24882355 19395Epoch: 2025-03-14T12:53Z
TLE epoch observation values (Epoch: 2025-03-14T12:53:31.375Z)
Latitude
-0.00003°
Longitude
-150.41951°
Altitude
179.787 km
Speed
7.816 km/s
True Right ascension
14h 21m 25s
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
07:12:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
247.998 km
Perigee altitude
169.242 km
Semi-major axis
6,586.757 km
Eccentricity
0.00598
Inclination
41.4837°
RAAN
215.3569°
Arg. of periapsis
311.4335°
True anomaly
48.65278°
Mean anomaly
48.14°
Eccentric anomaly
48.39613°
Mean motion
4.06009 °/min
Orbital period
88.67 mins
BSTAR
0.0006109
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Other satellites on launch #13 in the year 2024 (2024-01-17 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 E 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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