CZ-6A DEB, 56586

Orbit data source: Space-Track

CZ-6A DEB, 56586 is space debris in SSO originally from a launch on Fri, 11 Nov 2022 UTC launched from the Taiyaun Space Center, China (TSC). 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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Iframe URL

https://www.satcat.com/sats-embedded/56586?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

56586, 2022-151ADJ

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2022-11-11 (3 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago

0 CZ-6A DEB
1 56586U 22151ADJ 25349.59461800  .00012671  00000-0  19086-2 0  9990
2 56586  98.6490  41.6465 0059232 142.7471 217.7866 14.73356572151648

Epoch: 2025-12-15T14:16Z

TLE epoch observation values (Epoch: 2025-12-15T14:16:14.995Z)

Latitude

-0.00004°

Longitude

103.09309°

Altitude

686.362 km

Speed

7.496 km/s

True Right ascension

02h 46m 35s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

02:07:49

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

689.072 km

Perigee altitude

605.844 km

Semi-major axis

7,025.595 km

Eccentricity

0.00592

Inclination

98.649°

RAAN

41.6465°

Arg. of periapsis

142.7471°

True anomaly

217.37314°

Mean anomaly

217.7866°

Eccentric anomaly

217.57963°

Mean motion

3.68569 °/min

Orbital period

97.68 mins

BSTAR

0.0019086

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Other satellites on launch #151 in the year 2022 (2022-11-11 UTC)

CZ-6A DEB, 54906 (Decayed)

CZ-6A DEB, 55005 (Decayed)

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CZ-6A DEB 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	2025-12-18 04:19:17.943Z	202.049° SSW	2025-12-18 04:23:17.943Z	271.566° WNW	26.854°	2025-12-18 04:26:17.943Z	320.541° NNW
6 mins	2025-12-18 16:12:17.943Z	35.257° NE	2025-12-18 16:15:17.943Z	119.773° SE	34.992°	2025-12-18 16:18:17.943Z	171.44° S
6 mins	2025-12-19 03:10:17.943Z	132.042° SE	2025-12-19 03:13:17.943Z	52.929° ENE	33.902°	2025-12-19 03:16:17.943Z	3.591° NNE

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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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out CZ-6A DEB, 56586 on other resources

View CZ-6A DEB, 56586 on Heavens-Above

View CZ-6A DEB, 56586 on Keep Track

View CZ-6A DEB, 56586 on Celestrak

View CZ-6A DEB, 56586 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

CZ-6A DEB, 56586

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2025-12-15T14:16:14.995Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #151 in the year 2022 (2022-11-11 UTC)

CZ-6A DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-6A DEB, 56586 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago