CZ-6A DEB, 56270

Orbit data source: Space-Track

CZ-6A DEB, 56270 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/56270?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

56270, 2022-151ACN

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: 2 days ago

TLE from 2 days ago

0 CZ-6A DEB
1 56270U 22151ACN 26171.13319492  .00010287  00000-0  14712-2 0  9995
2 56270  98.6216 240.5039 0064437 258.5857 100.8108 14.75418686176340

Epoch: 2026-06-20T03:11Z

TLE epoch observation values (Epoch: 2026-06-20T03:11:48.041Z)

Latitude

0.00004°

Longitude

-75.79847°

Altitude

655.585 km

Speed

7.525 km/s

True Right ascension

16h 02m 00s

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

21:51:58

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

686.132 km

Perigee altitude

595.674 km

Semi-major axis

7,019.04 km

Eccentricity

0.00644

Inclination

98.6216°

RAAN

240.5039°

Arg. of periapsis

258.5857°

True anomaly

101.53498°

Mean anomaly

100.8108°

Eccentric anomaly

101.173°

Mean motion

3.69085 °/min

Orbital period

97.54 mins

BSTAR

0.0014712

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

CZ-6A DEB, 55528

CZ-6A DEB, 54606

CZ-6A DEB, 56246

CZ-6A DEB, 54906 (Decayed)

CZ-6A DEB, 55188 (Decayed)

CZ-6A DEB, 55184 (Decayed)

CZ-6A DEB, 54399 (Decayed)

CZ-6A DEB, 54495 (Decayed)

CZ-6A DEB, 54972 (Decayed)

CZ-6A DEB, 55893 (Decayed)

CZ-6A DEB, 56643 (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	2026-06-22 17:36:54.236Z	12.413° NNE	2026-06-22 17:40:54.236Z	278.965° WNW	44.936°	2026-06-22 17:44:54.236Z	196.389° SSW
8 mins	2026-06-23 04:33:54.236Z	161.782° S	2026-06-23 04:36:54.236Z	144.35° SSE	43.397°	2026-06-23 04:41:54.236Z	348.303° N

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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, 56270 on other resources

View CZ-6A DEB, 56270 on Heavens-Above

View CZ-6A DEB, 56270 on Keep Track

View CZ-6A DEB, 56270 on Celestrak

View CZ-6A DEB, 56270 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, 56270

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-06-20T03:11:48.041Z)

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, 56270 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago