CZ-6A DEB, 56256

Orbit data source: Space-Track

CZ-6A DEB, 56256 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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https://www.satcat.com/sats-embedded/56256?theme=dark&initialShowStats=false

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Identifier

56256, 2022-151ABY

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 (4 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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago

0 CZ-6A DEB
1 56256U 22151ABY 26264.12506001  .00001020  00000-0  20982-3 0  9997
2 56256  98.5647 331.3885 0140795 251.7665 106.8166 14.56963350185930

Epoch: 2026-09-21T03:00Z

TLE epoch observation values (Epoch: 2026-09-21T03:00:05.184Z)

Latitude

-0.00002°

Longitude

-73.64248°

Altitude

736.094 km

Speed

7.471 km/s

True Right ascension

22h 05m 33s

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

13:11:42

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

799.756 km

Perigee altitude

600.44 km

Semi-major axis

7,078.235 km

Eccentricity

0.01408

Inclination

98.5647°

RAAN

331.3885°

Arg. of periapsis

251.7665°

True anomaly

108.35299°

Mean anomaly

106.8166°

Eccentric anomaly

107.5856°

Mean motion

3.64465 °/min

Orbital period

98.77 mins

BSTAR

0.00020982

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

CZ-6A DEB, 54991 (Decayed)

CZ-6A DEB, 55203 (Decayed)

CZ-6A DEB, 54469 (Decayed)

CZ-6A DEB, 54635 (Decayed)

CZ-6A DEB, 54607 (Decayed)

CZ-6A DEB, 54310 (Decayed)

CZ-6A DEB, 54324 (Decayed)

CZ-6A DEB, 55531 (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.
8 mins	2026-09-22 03:51:19.218Z	131.431° SE	2026-09-22 03:55:19.218Z	72.25° E	36.897°	2026-09-22 03:59:19.218Z	8.281° NNE
7 mins	2026-09-22 05:30:19.218Z	220.252° SW	2026-09-22 05:33:19.218Z	268.138° W	26.854°	2026-09-22 05:37:19.218Z	320.487° NNW
8 mins	2026-09-22 17:30:19.218Z	14.364° NNE	2026-09-22 17:34:19.218Z	186.7° SSW	72.714°	2026-09-22 17:38:19.218Z	193.777° SSW

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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, 56256 on other resources

View CZ-6A DEB, 56256 on Heavens-Above

View CZ-6A DEB, 56256 on Keep Track

View CZ-6A DEB, 56256 on Celestrak

View CZ-6A DEB, 56256 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, 56256

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 17 hours ago

TLE from 17 hours ago

TLE epoch observation values (Epoch: 2026-09-21T03:00:05.184Z)

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, 56256 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 17 hours ago