CZ-6A DEB, 56665

Orbit data source: Space-Track

CZ-6A DEB, 56665 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/56665?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

56665, 2022-151AGR

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

Small (<0.1 m²)

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

TLE from 2 days ago

0 CZ-6A DEB
1 56665U 22151AGR 26171.21240943  .00002014  00000-0  39191-3 0  9994
2 56665  98.6995 257.4502 0122036 248.0046 110.8149 14.59715188172743

Epoch: 2026-06-20T05:05Z

TLE epoch observation values (Epoch: 2026-06-20T05:05:52.174Z)

Latitude

-0.00009°

Longitude

-87.44745°

Altitude

728.653 km

Speed

7.474 km/s

True Right ascension

17h 09m 48s

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

21:51:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

777.47 km

Perigee altitude

604.927 km

Semi-major axis

7,069.335 km

Eccentricity

0.0122

Inclination

98.6995°

RAAN

257.4502°

Arg. of periapsis

248.0046°

True anomaly

112.1149°

Mean anomaly

110.8149°

Eccentric anomaly

111.46562°

Mean motion

3.65153 °/min

Orbital period

98.59 mins

BSTAR

0.00039191

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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 18:32:53.034Z	18.527° NNE	2026-06-22 18:36:53.034Z	79.436° E	43.432°	2026-06-22 18:40:53.034Z	186.204° SSW
8 mins	2026-06-23 05:36:53.034Z	157.577° S	2026-06-23 05:39:53.034Z	125.286° SE	43.196°	2026-06-23 05:44:53.034Z	350.114° 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, 56665 on other resources

View CZ-6A DEB, 56665 on Heavens-Above

View CZ-6A DEB, 56665 on Keep Track

View CZ-6A DEB, 56665 on Celestrak

View CZ-6A DEB, 56665 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, 56665

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: 2026-06-20T05:05:52.174Z)

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, 56665 on other resources

Documentation

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