CZ-6A DEB, 56255

Orbit data source: Space-Track

CZ-6A DEB, 56255 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/56255?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

56255, 2022-151ABX

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 (3 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

Small (<0.1 m²)

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

TLE from 3 days ago

0 CZ-6A DEB
1 56255U 22151ABX 25347.19871502  .00005186  00000-0  33099-2 0  9994
2 56255  98.9036 319.9570 0140559 209.1004 150.2275 13.99216314137983

Epoch: 2025-12-13T04:46Z

TLE epoch observation values (Epoch: 2025-12-13T04:46:08.977Z)

Latitude

-0°

Longitude

166.29017°

Altitude

988.51 km

Speed

7.312 km/s

True Right ascension

21h 19m 49s

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

08:25:54

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

995.917 km

Perigee altitude

791.493 km

Semi-major axis

7,271.842 km

Eccentricity

0.01406

Inclination

98.9036°

RAAN

319.957°

Arg. of periapsis

209.1004°

True anomaly

151.01525°

Mean anomaly

150.2275°

Eccentric anomaly

150.62257°

Mean motion

3.50007 °/min

Orbital period

102.86 mins

BSTAR

0.0033099

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

YUNHAI 3, 54235

CZ-6A DEB, 54618 (Decayed)

CZ-6A DEB, 57577 (Decayed)

CZ-6A DEB, 56235 (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.
9 mins	2025-12-16 10:36:12.695Z	32.572° NE	2025-12-16 10:40:12.695Z	84.552° E	31.443°	2025-12-16 10:45:12.695Z	163.668° S
7 mins	2025-12-16 12:19:12.695Z	338.353° N	2025-12-16 12:22:12.695Z	293.731° NW	24.545°	2025-12-16 12:26:12.695Z	241.595° WSW
10 mins	2025-12-16 22:08:12.695Z	157.172° SSE	2025-12-16 22:12:12.695Z	117.198° SE	43.779°	2025-12-16 22:18:12.695Z	349.616° N
5 mins	2025-12-16 23:53:12.695Z	252.297° W	2025-12-16 23:55:12.695Z	274.34° WNW	15.163°	2025-12-16 23:58:12.695Z	304.192° NW

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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, 56255 on other resources

View CZ-6A DEB, 56255 on Heavens-Above

View CZ-6A DEB, 56255 on Keep Track

View CZ-6A DEB, 56255 on Celestrak

View CZ-6A DEB, 56255 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, 56255

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: 2025-12-13T04:46:08.977Z)

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, 56255 on other resources

Documentation

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