CZ-6A DEB, 54565

Orbit data source: Space-Track

CZ-6A DEB, 54565 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/54565?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

54565, 2022-151LR

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: 1 day ago

TLE from 1 day ago

0 CZ-6A DEB
1 54565U 22151LR  26235.12554309  .00008517  00000-0  13783-2 0  9998
2 54565  98.6274 304.6869 0092563  89.7425 271.4385 14.68700921199871

Epoch: 2026-08-23T03:00Z

TLE epoch observation values (Epoch: 2026-08-23T03:00:46.922Z)

Latitude

-0.00004°

Longitude

-71.93469°

Altitude

667.169 km

Speed

7.524 km/s

True Right ascension

20h 18m 44s

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

02:08:38

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

727.476 km

Perigee altitude

597.139 km

Semi-major axis

7,040.445 km

Eccentricity

0.00926

Inclination

98.6274°

RAAN

304.6869°

Arg. of periapsis

89.7425°

True anomaly

270.37789°

Mean anomaly

271.4385°

Eccentric anomaly

270.90822°

Mean motion

3.67403 °/min

Orbital period

97.98 mins

BSTAR

0.0013783

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

CZ-6A DEB, 54889 (Decayed)

CZ-6A DEB, 56272

CZ-6A DEB, 56276

CZ-6A DEB, 54465 (Decayed)

CZ-6A DEB, 54531 (Decayed)

CZ-6A DEB, 56621

CZ-6A DEB, 56651

CZ-6A DEB, 55889 (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	2026-08-24 17:11:09.647Z	29.449° NE	2026-08-24 17:15:09.647Z	109.441° ESE	33.876°	2026-08-24 17:18:09.647Z	166.763° S
4 mins	2026-08-24 18:50:09.647Z	317.793° NNW	2026-08-24 18:51:09.647Z	301.658° NW	15.878°	2026-08-24 18:54:09.647Z	256.844° W
6 mins	2026-08-25 04:12:09.647Z	135.097° SSE	2026-08-25 04:15:09.647Z	72.528° E	33.147°	2026-08-25 04:18:09.647Z	7.63° 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, 54565 on other resources

View CZ-6A DEB, 54565 on Heavens-Above

View CZ-6A DEB, 54565 on Keep Track

View CZ-6A DEB, 54565 on Celestrak

View CZ-6A DEB, 54565 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, 54565

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-08-23T03:00:46.922Z)

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, 54565 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago