CZ-6A DEB, 60900

Orbit data source: Space-Track

CZ-6A DEB, 60900 is space debris in LEO originally from a launch on Tue, 06 Aug 2024 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/60900?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60900, 2024-140LF

Orbit

LEO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2024-08-06 (2 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: 15 hours ago

TLE from 15 hours ago

0 CZ-6A DEB
1 60900U 24140LF  26171.21076813  .00000215  00000-0  83584-4 0  9991
2 60900  88.9169 266.7002 0019097 113.3768 246.9436 14.26163465 95585

Epoch: 2026-06-20T05:03Z

TLE epoch observation values (Epoch: 2026-06-20T05:03:30.366Z)

Latitude

-0.00009°

Longitude

-77.60498°

Altitude

813.041 km

Speed

7.444 km/s

True Right ascension

17h 46m 48s

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

07:23:52

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

815.237 km

Perigee altitude

787.815 km

Semi-major axis

7,179.663 km

Eccentricity

0.00191

Inclination

88.9169°

RAAN

266.7002°

Arg. of periapsis

113.3768°

True anomaly

246.74243°

Mean anomaly

246.9436°

Eccentric anomaly

246.843°

Mean motion

3.56769 °/min

Orbital period

100.91 mins

BSTAR

0.000083584

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Other satellites on launch #140 in the year 2024 (2024-08-06 UTC)

CZ-6A DEB, 60882

CZ-6A DEB, 61384 (Decayed)

CZ-6A DEB, 60744 (Decayed)

CZ-6A DEB, 60849

CZ-6A DEB, 60885

CZ-6A DEB, 61344 (Decayed)

CZ-6A DEB, 60711

CZ-6A DEB, 60799

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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	2026-06-21 06:26:06.418Z	158.559° S	2026-06-21 06:30:06.418Z	92.631° ESE	39.458°	2026-06-21 06:35:06.418Z	9.041° NNE
4 mins	2026-06-21 08:10:06.418Z	261.631° W	2026-06-21 08:11:06.418Z	274.646° WNW	15.7°	2026-06-21 08:14:06.418Z	312.678° NW
8 mins	2026-06-21 18:42:06.418Z	359.237° N	2026-06-21 18:45:06.418Z	341.046° N	44.377°	2026-06-21 18:50:06.418Z	184.327° 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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Check out CZ-6A DEB, 60900 on other resources

View CZ-6A DEB, 60900 on Heavens-Above

View CZ-6A DEB, 60900 on Keep Track

View CZ-6A DEB, 60900 on Celestrak

View CZ-6A DEB, 60900 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, 60900

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: 2026-06-20T05:03:30.366Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #140 in the year 2024 (2024-08-06 UTC)

CZ-6A DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-6A DEB, 60900 on other resources

Documentation

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