CZ-6A DEB, 56684

Orbit data source: Space-Track

CZ-6A DEB, 56684 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/56684?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

56684, 2022-151AHL

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: 2 days ago

TLE from 2 days ago

0 CZ-6A DEB
1 56684U 22151AHL 26128.66919982  .00001558  00000-0  10192-2 0  9993
2 56684  98.9167 108.7010 0105828 155.6310 204.9912 14.00929780153289

Epoch: 2026-05-08T16:03Z

TLE epoch observation values (Epoch: 2026-05-08T16:03:38.864Z)

Latitude

0.00004°

Longitude

1.29139°

Altitude

963.338 km

Speed

7.335 km/s

True Right ascension

07h 14m 48s

True Declination

0° 00' 00"

Sunlit

Object was in daylight 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

19:53:20

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

964.665 km

Perigee altitude

810.877 km

Semi-major axis

7,265.908 km

Eccentricity

0.01058

Inclination

98.9167°

RAAN

108.701°

Arg. of periapsis

155.631°

True anomaly

204.48494°

Mean anomaly

204.9912°

Eccentric anomaly

204.73747°

Mean motion

3.50436 °/min

Orbital period

102.73 mins

BSTAR

0.0010192

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

CZ-6A DEB, 54980 (Decayed)

CZ-6A DEB, 55184 (Decayed)

CZ-6A DEB, 55518 (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	2026-05-10 21:21:39.277Z	104.673° ESE	2026-05-10 21:24:39.277Z	68.513° E	20.896°	2026-05-10 21:28:39.277Z	19.049° NNE
9 mins	2026-05-10 23:01:39.277Z	186.674° SSW	2026-05-10 23:05:39.277Z	242.795° WSW	38.462°	2026-05-10 23:10:39.277Z	333.107° NNW
9 mins	2026-05-11 11:30:39.277Z	17.025° NNE	2026-05-11 11:34:39.277Z	149.43° SSE	44.424°	2026-05-11 11:39:39.277Z	191.92° 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, 56684 on other resources

View CZ-6A DEB, 56684 on Heavens-Above

View CZ-6A DEB, 56684 on Keep Track

View CZ-6A DEB, 56684 on Celestrak

View CZ-6A DEB, 56684 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, 56684

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: 2026-05-08T16:03:38.864Z)

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, 56684 on other resources

Documentation

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