ZQ-2 R/B, 58556 (Decayed)
Orbit data source: Space-Track
ZQ-2 R/B, 58556 was space debris in LEO originally from a launch on Fri, 08 Dec 2023 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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58556 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
5 months ago
Origin
Landspace (CN / PRC)Manufacturer
Lanjian Hangtian
Mission
Decayed spacecraft
Bus & Motor
ZQ-2 ST 2, Unknown motor
Mass
~5,000 kg wet, ~5,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 6.0 m
Radar Cross Section
35.980 m², Large (>1 m²)
Expand to show TLE details & history
TLE from 5 months ago
0 OBJECT D
1 58556U 23193D 25033.22823895 .13754771 24818-5 24476-3 0 9998
2 58556 97.2212 58.1933 0007595 267.0586 161.2014 16.47442894 65659Epoch: 2025-02-02T05:28Z
TLE epoch observation values (Epoch: 2025-02-02T05:28:39.845Z)
Latitude
67.26532°
Longitude
-174.13424°
Altitude
162.45 km
Speed
7.812 km/s
True Right ascension
02h 42m 47s
True Declination
67° 07' 52"
Sunlit
Visualization orbit readout
No trajectory is available.
Visualization observer readout
No trajectory is available.
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Other satellites on launch #193 in the year 2023 (2023-12-08 UTC)
ZQ-2 R/B Visibility
Observer location: undefined°, undefined°
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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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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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Authenticating...
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