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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ISO8601 Format

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: 9 hours ago

TLE from 9 hours ago

0 CZ-6A DEB
1 54569U 22151LV  26237.19802464  .00115350  00000-0  51105-2 0  9993
2 54569  98.6238 335.0000 0022937 343.2577  16.7895 15.20888191201969

Epoch: 2026-08-25T04:45Z

TLE epoch observation values (Epoch: 2026-08-25T04:45:09.328Z)

Latitude

-0.00007°

Longitude

-69.75768°

Altitude

491.103 km

Speed

7.628 km/s

True Right ascension

22h 20m 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

05:11:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

515.958 km

Perigee altitude

484.404 km

Semi-major axis

6,878.318 km

Eccentricity

0.00229

Inclination

98.6238°

RAAN

335°

Arg. of periapsis

343.2577°

True anomaly

16.86563°

Mean anomaly

16.7895°

Eccentric anomaly

16.82754°

Mean motion

3.80469 °/min

Orbital period

94.62 mins

BSTAR

0.0051105

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

CZ-6A DEB, 56596

CZ-6A DEB, 54408 (Decayed)

CZ-6A DEB, 54427

CZ-6A DEB, 54477 (Decayed)

CZ-6A DEB, 54607 (Decayed)

CZ-6A DEB, 55226 (Decayed)

CZ-6A DEB, 55558 (Decayed)

CZ-6A DEB, 54985 (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	2026-08-25 19:31:22.453Z	14.723° NNE	2026-08-25 19:34:22.453Z	50.814° ENE	44.808°	2026-08-25 19:37:22.453Z	192.723° SSW
4 mins	2026-08-26 06:10:22.453Z	120.292° SE	2026-08-26 06:11:22.453Z	91.069° ESE	30.91°	2026-08-26 06:14:22.453Z	8.422° 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: 9 hours ago

TLE from 9 hours ago

TLE epoch observation values (Epoch: 2026-08-25T04:45:09.328Z)

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: 9 hours ago