CZ-6A DEB, 60960

Orbit data source: Space-Track

CZ-6A DEB, 60960 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/60960?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60960, 2024-140LK

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, 0.2 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 CZ-6A DEB
1 60960U 24140LK  26113.43681534  .00000714  00000-0  32158-3 0  9993
2 60960  89.0717 286.5031 0047092 345.6004  14.3840 14.20682077 86814

Epoch: 2026-04-23T10:29Z

TLE epoch observation values (Epoch: 2026-04-23T10:29:00.845Z)

Latitude

-0.00011°

Longitude

-82.23433°

Altitude

793.256 km

Speed

7.474 km/s

True Right ascension

19h 06m 00s

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

17:11:40

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

853.894 km

Perigee altitude

786.099 km

Semi-major axis

7,198.134 km

Eccentricity

0.00471

Inclination

89.0717°

RAAN

286.5031°

Arg. of periapsis

345.6004°

True anomaly

14.51882°

Mean anomaly

14.384°

Eccentric anomaly

14.45133°

Mean motion

3.55397 °/min

Orbital period

101.3 mins

BSTAR

0.00032158

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

CZ-6A DEB, 61798

CZ-6A DEB, 61353 (Decayed)

CZ-6A DEB, 60642 (Decayed)

CZ-6A DEB, 61465 (Decayed)

CZ-6A DEB, 60629 (Decayed)

CZ-6A DEB, 61392 (Decayed)

CZ-6A DEB, 61140 (Decayed)

CZ-6A DEB, 60851 (Decayed)

CZ-6A DEB, 61148 (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	2026-04-24 11:57:21.029Z	179.735° S	2026-04-24 12:01:21.029Z	220.961° SW	44.826°	2026-04-24 12:06:21.029Z	357.854° N
6 mins	2026-04-24 22:35:21.029Z	44.853° NE	2026-04-24 22:38:21.029Z	84.357° E	19.178°	2026-04-24 22:41:21.029Z	120.835° SE
9 mins	2026-04-25 00:15:21.029Z	346.111° N	2026-04-25 00:19:21.029Z	287.083° WNW	36.998°	2026-04-25 00:24:21.029Z	205.3° SW

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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, 60960 on other resources

View CZ-6A DEB, 60960 on Heavens-Above

View CZ-6A DEB, 60960 on Keep Track

View CZ-6A DEB, 60960 on Celestrak

View CZ-6A DEB, 60960 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, 60960

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-04-23T10:29:00.845Z)

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, 60960 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago