CZ-6A DEB, 54466

Orbit data source: Space-Track

CZ-6A DEB, 54466 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/54466?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

54466, 2022-151GS

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, 0.2 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

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

TLE from 2 days ago

0 CZ-6A DEB
1 54466U 22151GS  26296.98240290  .00000951  00000-0  48829-3 0  9994
2 54466  98.8234 307.9146 0028156 295.7954  64.0317 14.17551934203639

Epoch: 2026-10-23T23:34Z

TLE epoch observation values (Epoch: 2026-10-23T23:34:39.610Z)

Latitude

0.00003°

Longitude

-78.14558°

Altitude

827.705 km

Speed

7.444 km/s

True Right ascension

20h 31m 39s

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

07:42:00

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

851.109 km

Perigee altitude

810.514 km

Semi-major axis

7,208.948 km

Eccentricity

0.00282

Inclination

98.8234°

RAAN

307.9146°

Arg. of periapsis

295.7954°

True anomaly

64.32222°

Mean anomaly

64.0317°

Eccentric anomaly

64.17691°

Mean motion

3.54597 °/min

Orbital period

101.52 mins

BSTAR

0.00048829

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

CZ-6A DEB, 56603 (Decayed)

CZ-6A DEB, 56617 (Decayed)

CZ-6A DEB, 54430 (Decayed)

CZ-6A DEB, 57577 (Decayed)

CZ-6A DEB, 56643 (Decayed)

CZ-6A DEB, 56248

CZ-6A DEB, 54920

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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.
10 mins	2026-10-25 13:25:50.546Z	23.851° NE	2026-10-25 13:30:50.546Z	116.845° SE	57.137°	2026-10-25 13:35:50.546Z	180.032° SSW
6 mins	2026-10-25 15:07:50.546Z	330.197° NNW	2026-10-25 15:10:50.546Z	290.717° WNW	19.449°	2026-10-25 15:13:50.546Z	256.025° W
9 mins	2026-10-26 00:49:50.546Z	165.564° S	2026-10-26 00:53:50.546Z	337.515° N	82.365°	2026-10-26 00:58:50.546Z	346.149° 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, 54466 on other resources

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View CZ-6A DEB, 54466 on Keep Track

View CZ-6A DEB, 54466 on Celestrak

View CZ-6A DEB, 54466 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, 54466

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: 2026-10-23T23:34:39.610Z)

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, 54466 on other resources

Documentation

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