CZ-6A DEB, 61320

Orbit data source: Space-Track

CZ-6A DEB, 61320 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/61320?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61320, 2024-140UH

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

Small (<0.1 m²)

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

TLE from 2 days ago

0 CZ-6A DEB
1 61320U 24140UH  26112.72787707  .00000294  00000-0  11696-3 0  9991
2 61320  88.9932 280.1282 0014990 349.0707  11.0158 14.26030583 85662

Epoch: 2026-04-22T17:28Z

TLE epoch observation values (Epoch: 2026-04-22T17:28:08.578Z)

Latitude

-0.00009°

Longitude

167.30731°

Altitude

797.521 km

Speed

7.46 km/s

True Right ascension

18h 40m 30s

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

17:11:04

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

812.735 km

Perigee altitude

791.209 km

Semi-major axis

7,180.109 km

Eccentricity

0.0015

Inclination

88.9932°

RAAN

280.1282°

Arg. of periapsis

349.0707°

True anomaly

11.04868°

Mean anomaly

11.0158°

Eccentric anomaly

11.03224°

Mean motion

3.56736 °/min

Orbital period

100.92 mins

BSTAR

0.00011696

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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.
8 mins	2026-04-24 11:41:44.787Z	189.459° SSW	2026-04-24 11:45:44.787Z	300.026° NW	42.707°	2026-04-24 11:49:44.787Z	352.747° N
6 mins	2026-04-24 22:16:44.787Z	41.577° NE	2026-04-24 22:19:44.787Z	84.146° E	21.072°	2026-04-24 22:22:44.787Z	124.286° SE
8 mins	2026-04-24 23:56:44.787Z	341.074° N	2026-04-25 00:00:44.787Z	275.317° WNW	33.391°	2026-04-25 00:04:44.787Z	213.158° 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, 61320 on other resources

View CZ-6A DEB, 61320 on Heavens-Above

View CZ-6A DEB, 61320 on Keep Track

View CZ-6A DEB, 61320 on Celestrak

View CZ-6A DEB, 61320 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, 61320

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: 2026-04-22T17:28:08.578Z)

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, 61320 on other resources

Documentation

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