CZ-6A DEB, 54616

Orbit data source: Space-Track

CZ-6A DEB, 54616 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/54616?theme=dark&initialShowStats=false

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Identifier

54616, 2022-151NS

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: 15 hours ago

TLE from 15 hours ago

0 CZ-6A DEB
1 54616U 22151NS  25354.85560163  .00000988  00000-0  54447-3 0  9998
2 54616  98.8211 351.2180 0056953 138.8809 221.6676 14.12999506158659

Epoch: 2025-12-20T20:32Z

TLE epoch observation values (Epoch: 2025-12-20T20:32:03.980Z)

Latitude

-0.00005°

Longitude

-46.47499°

Altitude

882.884 km

Speed

7.395 km/s

True Right ascension

23h 24m 52s

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

10:41:30

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

887.444 km

Perigee altitude

805.153 km

Semi-major axis

7,224.436 km

Eccentricity

0.0057

Inclination

98.8211°

RAAN

351.218°

Arg. of periapsis

138.8809°

True anomaly

221.23602°

Mean anomaly

221.6676°

Eccentric anomaly

221.45158°

Mean motion

3.53458 °/min

Orbital period

101.85 mins

BSTAR

0.00054447

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

YUNHAI 3, 54235

CZ-6A DEB, 55880 (Decayed)

CZ-6A DEB, 54502 (Decayed)

CZ-6A DEB, 54979 (Decayed)

CZ-6A DEB, 55188 (Decayed)

CZ-6A DEB, 54324 (Decayed)

CZ-6A DEB, 54319 (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	2025-12-21 12:24:47.594Z	25.974° NE	2025-12-21 12:29:47.594Z	114.367° SE	37.345°	2025-12-21 12:33:47.594Z	173.295° S
5 mins	2025-12-21 14:07:47.594Z	324.303° NNW	2025-12-21 14:09:47.594Z	295.408° NW	19.071°	2025-12-21 14:12:47.594Z	256.512° W
9 mins	2025-12-21 23:50:47.594Z	163.317° S	2025-12-21 23:54:47.594Z	146.364° SSE	44.658°	2025-12-21 23:59:47.594Z	347.133° 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, 54616 on other resources

View CZ-6A DEB, 54616 on Heavens-Above

View CZ-6A DEB, 54616 on Keep Track

View CZ-6A DEB, 54616 on Celestrak

View CZ-6A DEB, 54616 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, 54616

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 15 hours ago

TLE from 15 hours ago

TLE epoch observation values (Epoch: 2025-12-20T20:32:03.980Z)

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, 54616 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 15 hours ago