CZ-6A DEB, 56680

Orbit data source: Space-Track

CZ-6A DEB, 56680 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/56680?theme=dark&initialShowStats=false

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Identifier

56680, 2022-151AHG

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 56680U 22151AHG 26171.44180221  .00004461  00000-0  82322-3 0  9990
2 56680  98.6135 233.0137 0078947 283.0269  76.2127 14.64022653171415

Epoch: 2026-06-20T10:36Z

TLE epoch observation values (Epoch: 2026-06-20T10:36:11.710Z)

Latitude

-0.00006°

Longitude

165.30854°

Altitude

670.326 km

Speed

7.529 km/s

True Right ascension

15h 32m 03s

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

21:52:16

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

733.011 km

Perigee altitude

621.609 km

Semi-major axis

7,055.447 km

Eccentricity

0.00789

Inclination

98.6135°

RAAN

233.0137°

Arg. of periapsis

283.0269°

True anomaly

77.09334°

Mean anomaly

76.2127°

Eccentric anomaly

76.65282°

Mean motion

3.66232 °/min

Orbital period

98.3 mins

BSTAR

0.00082322

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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.
7 mins	2026-06-22 17:19:11.467Z	2.342° NNE	2026-06-22 17:22:11.467Z	291.24° WNW	42.015°	2026-06-22 17:26:11.467Z	207.725° SW
8 mins	2026-06-23 04:20:11.467Z	179.019° S	2026-06-23 04:24:11.467Z	289.514° WNW	41.172°	2026-06-23 04:28:11.467Z	339.674° 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, 56680 on other resources

View CZ-6A DEB, 56680 on Heavens-Above

View CZ-6A DEB, 56680 on Keep Track

View CZ-6A DEB, 56680 on Celestrak

View CZ-6A DEB, 56680 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, 56680

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: 2026-06-20T10:36:11.710Z)

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, 56680 on other resources

Documentation

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