CZ-6A DEB, 68406

Orbit data source: Space-Track

CZ-6A DEB, 68406 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/68406?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

68406, 2022-151AJH

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: 16 hours ago

TLE from 16 hours ago

0 CZ-6A DEB
1 68406U 22151AJH 26236.33101750  .00007603  00000-0  14125-2 0  9995
2 68406  99.1324  17.1569 0074472 143.1475 217.4875 14.63709023179468

Epoch: 2026-08-24T07:56Z

TLE epoch observation values (Epoch: 2026-08-24T07:56:39.911Z)

Latitude

-0.0001°

Longitude

-74.62364°

Altitude

726.051 km

Speed

7.47 km/s

True Right ascension

01h 08m 37s

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

14:51:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

730.896 km

Perigee altitude

625.793 km

Semi-major axis

7,056.482 km

Eccentricity

0.00745

Inclination

99.1324°

RAAN

17.1569°

Arg. of periapsis

143.1475°

True anomaly

216.97196°

Mean anomaly

217.4875°

Eccentric anomaly

217.22935°

Mean motion

3.66152 °/min

Orbital period

98.32 mins

BSTAR

0.0014125

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

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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	2026-08-25 08:41:50.820Z	124.361° SE	2026-08-25 08:44:50.820Z	74.045° E	27.971°	2026-08-25 08:48:50.820Z	7.859° NNE
6 mins	2026-08-25 10:19:50.820Z	222.019° SW	2026-08-25 10:21:50.820Z	254.966° W	22.46°	2026-08-25 10:25:50.820Z	316.852° NNW
7 mins	2026-08-25 22:15:50.820Z	23.379° NE	2026-08-25 22:18:50.820Z	107.488° ESE	42.633°	2026-08-25 22:22:50.820Z	185.657° SSW

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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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CZ-6A DEB, 68406

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 16 hours ago

TLE from 16 hours ago

TLE epoch observation values (Epoch: 2026-08-24T07:56:39.911Z)

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, 68406 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 16 hours ago