CZ-6A DEB, 54569

Orbit data source: Space-Track

CZ-6A DEB, 54569 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/54569?theme=dark&initialShowStats=false

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Identifier

54569, 2022-151LV

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: 3 days ago

TLE from 3 days ago

0 CZ-6A DEB
1 54569U 22151LV  26170.77441267  .00063048  00000-0  37837-2 0  9995
2 54569  98.6312 259.6307 0036339 210.8679 149.0411 15.10110087191903

Epoch: 2026-06-19T18:35Z

TLE epoch observation values (Epoch: 2026-06-19T18:35:09.254Z)

Latitude

-0.00004°

Longitude

72.84358°

Altitude

560.477 km

Speed

7.569 km/s

True Right ascension

17h 18m 31s

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

23:18:43

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

558.013 km

Perigee altitude

507.785 km

Semi-major axis

6,911.036 km

Eccentricity

0.00363

Inclination

98.6312°

RAAN

259.6307°

Arg. of periapsis

210.8679°

True anomaly

149.25448°

Mean anomaly

149.0411°

Eccentric anomaly

149.14787°

Mean motion

3.77771 °/min

Orbital period

95.3 mins

BSTAR

0.0037837

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

CZ-6A DEB, 54317 (Decayed)

CZ-6A DEB, 54438 (Decayed)

CZ-6A DEB, 55553 (Decayed)

CZ-6A DEB, 56603 (Decayed)

CZ-6A DEB, 55531 (Decayed)

CZ-6A DEB, 54483 (Decayed)

CZ-6A DEB, 54913 (Decayed)

CZ-6A DEB, 55188 (Decayed)

CZ-6A DEB, 55184 (Decayed)

CZ-6A DEB, 54555

CZ-6A DEB, 54556 (Decayed)

CZ-6A DEB, 54399 (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.
6 mins	2026-06-22 18:42:24.937Z	22.331° NNE	2026-06-22 18:45:24.937Z	88.099° E	41.176°	2026-06-22 18:48:24.937Z	180.753° SSW
5 mins	2026-06-23 05:25:24.937Z	120.804° SE	2026-06-23 05:27:24.937Z	67.485° ENE	30.053°	2026-06-23 05:30:24.937Z	8.051° NNE

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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, 54569 on other resources

View CZ-6A DEB, 54569 on Heavens-Above

View CZ-6A DEB, 54569 on Keep Track

View CZ-6A DEB, 54569 on Celestrak

View CZ-6A DEB, 54569 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, 54569

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-06-19T18:35:09.254Z)

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, 54569 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago