CZ-6A DEB, 54598

Orbit data source: Space-Track

CZ-6A DEB, 54598 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/54598?theme=dark&initialShowStats=false

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Identifier

54598, 2022-151MY

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, 0.1 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 54598U 22151MY  26171.27827388  .00027407  00000-0  28524-2 0  9997
2 54598  98.8989 291.8402 0042286 228.5228 131.2353 14.89142203191150

Epoch: 2026-06-20T06:40Z

TLE epoch observation values (Epoch: 2026-06-20T06:40:42.863Z)

Latitude

0.00004°

Longitude

-76.83359°

Altitude

623.143 km

Speed

7.537 km/s

True Right ascension

19h 27m 21s

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

21:24:31

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

627.189 km

Perigee altitude

568.193 km

Semi-major axis

6,975.828 km

Eccentricity

0.00423

Inclination

98.8989°

RAAN

291.8402°

Arg. of periapsis

228.5228°

True anomaly

131.59843°

Mean anomaly

131.2353°

Eccentric anomaly

131.41699°

Mean motion

3.7252 °/min

Orbital period

96.64 mins

BSTAR

0.0028524

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

CZ-6A DEB, 56278

CZ-6A DEB, 55184 (Decayed)

CZ-6A DEB, 55231

CZ-6A DEB, 54267

CZ-6A DEB, 55865 (Decayed)

CZ-6A DEB, 55193 (Decayed)

CZ-6A DEB, 55188 (Decayed)

CZ-6A DEB, 54602 (Decayed)

CZ-6A DEB, 54399 (Decayed)

CZ-6A DEB, 54495 (Decayed)

CZ-6A DEB, 54524

CZ-6A DEB, 54273

CZ-6A DEB, 54428

CZ-6A DEB, 54435 (Decayed)

CZ-6A DEB, 54504

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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	2026-06-22 20:31:31.562Z	30.32° NE	2026-06-22 20:35:31.562Z	106.705° ESE	32.126°	2026-06-22 20:38:31.562Z	165.223° S
6 mins	2026-06-23 07:23:31.562Z	122.46° SE	2026-06-23 07:26:31.562Z	58.03° ENE	28.059°	2026-06-23 07:29:31.562Z	9.138° NNE
5 mins	2026-06-23 08:59:31.562Z	225.941° WSW	2026-06-23 09:01:31.562Z	259.716° W	19.925°	2026-06-23 09:04:31.562Z	309.025° 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, 54598 on other resources

View CZ-6A DEB, 54598 on Heavens-Above

View CZ-6A DEB, 54598 on Keep Track

View CZ-6A DEB, 54598 on Celestrak

View CZ-6A DEB, 54598 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, 54598

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: 2026-06-20T06:40:42.863Z)

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, 54598 on other resources

Documentation

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