CZ-6A DEB, 54500

Orbit data source: Space-Track

CZ-6A DEB, 54500 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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Iframe URL

https://www.satcat.com/sats-embedded/54500?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

54500, 2022-151JC

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, 1.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago

0 CZ-6A DEB
1 54500U 22151JC  26193.58990624  .00001350  00000-0  51247-3 0  9990
2 54500  98.8774 239.7586 0111337  94.2819 267.1094 14.29351089190212

Epoch: 2026-07-12T14:09Z

TLE epoch observation values (Epoch: 2026-07-12T14:09:27.899Z)

Latitude

0.00001°

Longitude

96.90576°

Altitude

801.737 km

Speed

7.45 km/s

True Right ascension

15h 59m 02s

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

22:00:23

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

870.874 km

Perigee altitude

711.235 km

Semi-major axis

7,169.191 km

Eccentricity

0.01113

Inclination

98.8774°

RAAN

239.7586°

Arg. of periapsis

94.2819°

True anomaly

265.83619°

Mean anomaly

267.1094°

Eccentric anomaly

266.47269°

Mean motion

3.57551 °/min

Orbital period

100.68 mins

BSTAR

0.00051247

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

CZ-6A DEB, 54490 (Decayed)

CZ-6A DEB, 54985 (Decayed)

CZ-6A DEB, 55224 (Decayed)

CZ-6A DEB, 54349

CZ-6A DEB, 54387 (Decayed)

CZ-6A DEB, 54583

CZ-6A DEB, 56261

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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.
9 mins	2026-07-13 15:55:43.380Z	17.696° NNE	2026-07-13 15:59:43.380Z	68.373° E	43.79°	2026-07-13 16:04:43.380Z	189.359° SSW
8 mins	2026-07-14 03:14:43.380Z	175.228° S	2026-07-14 03:17:43.380Z	215.592° SW	42.46°	2026-07-14 03:22:43.380Z	341.367° 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, 54500 on other resources

View CZ-6A DEB, 54500 on Heavens-Above

View CZ-6A DEB, 54500 on Keep Track

View CZ-6A DEB, 54500 on Celestrak

View CZ-6A DEB, 54500 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, 54500

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 19 hours ago

TLE from 19 hours ago

TLE epoch observation values (Epoch: 2026-07-12T14:09:27.899Z)

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, 54500 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 19 hours ago