CZ-6A DEB, 60838

Orbit data source: Space-Track

CZ-6A DEB, 60838 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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Iframe URL

https://www.satcat.com/sats-embedded/60838?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60838, 2024-140HR

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: 13 hours ago

TLE from 13 hours ago

0 CZ-6A DEB
1 60838U 24140HR  26171.32315514  .00002200  00000-0  53030-3 0  9995
2 60838  89.0817 277.4079 0068889 234.1404 125.3394 14.51500132 97895

Epoch: 2026-06-20T07:45Z

TLE epoch observation values (Epoch: 2026-06-20T07:45:20.604Z)

Latitude

0.00002°

Longitude

-107.46738°

Altitude

752.367 km

Speed

7.463 km/s

True Right ascension

18h 29m 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

07:13:51

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

766.541 km

Perigee altitude

668.776 km

Semi-major axis

7,095.796 km

Eccentricity

0.00689

Inclination

89.0817°

RAAN

277.4079°

Arg. of periapsis

234.1404°

True anomaly

125.98015°

Mean anomaly

125.3394°

Eccentric anomaly

125.66009°

Mean motion

3.63113 °/min

Orbital period

99.14 mins

BSTAR

0.0005303

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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, 61344 (Decayed)

CZ-6A DEB, 60711

CZ-6A DEB, 61310 (Decayed)

QIANFAN-4, 60382

QIANFAN-5, 60383

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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 07:02:07.104Z	153.845° SSE	2026-06-21 07:06:07.104Z	93.345° ESE	36.15°	2026-06-21 07:11:07.104Z	11.634° NNE
5 mins	2026-06-21 08:44:07.104Z	255.424° W	2026-06-21 08:46:07.104Z	284.481° WNW	17.756°	2026-06-21 08:49:07.104Z	321.789° NNW
7 mins	2026-06-21 19:06:07.104Z	15.747° NNE	2026-06-21 19:09:07.104Z	92.706° ESE	40.821°	2026-06-21 19:13:07.104Z	167.177° S

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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, 60838 on other resources

View CZ-6A DEB, 60838 on Heavens-Above

View CZ-6A DEB, 60838 on Keep Track

View CZ-6A DEB, 60838 on Celestrak

View CZ-6A DEB, 60838 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, 60838

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 13 hours ago

TLE from 13 hours ago

TLE epoch observation values (Epoch: 2026-06-20T07:45:20.604Z)

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, 60838 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 13 hours ago