CZ-6A DEB, 61145

Orbit data source: Space-Track

CZ-6A DEB, 61145 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/61145?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61145, 2024-140QP

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: 1 day ago

TLE from 1 day ago

0 CZ-6A DEB
1 61145U 24140QP  26170.71333702  .00020488  00000-0  25402-2 0  9997
2 61145  88.9310 263.2226 0053327 222.9869 136.7184 14.81558024 97575

Epoch: 2026-06-19T17:07Z

TLE epoch observation values (Epoch: 2026-06-19T17:07:12.318Z)

Latitude

0°

Longitude

98.48291°

Altitude

654.835 km

Speed

7.515 km/s

True Right ascension

17h 32m 53s

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

07:24:32

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

658.6 km

Perigee altitude

583.949 km

Semi-major axis

6,999.411 km

Eccentricity

0.00533

Inclination

88.931°

RAAN

263.2226°

Arg. of periapsis

222.9869°

True anomaly

137.13532°

Mean anomaly

136.7184°

Eccentric anomaly

136.92706°

Mean motion

3.70639 °/min

Orbital period

97.13 mins

BSTAR

0.0025402

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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.
8 mins	2026-06-21 06:30:45.636Z	175.096° S	2026-06-21 06:34:45.636Z	145.645° SSE	44.371°	2026-06-21 06:38:45.636Z	1.028° NNE
7 mins	2026-06-21 18:19:45.636Z	5.29° NNE	2026-06-21 18:22:45.636Z	49.829° ENE	43.816°	2026-06-21 18:26:45.636Z	176.67° 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, 61145 on other resources

View CZ-6A DEB, 61145 on Heavens-Above

View CZ-6A DEB, 61145 on Keep Track

View CZ-6A DEB, 61145 on Celestrak

View CZ-6A DEB, 61145 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, 61145

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: 2026-06-19T17:07:12.318Z)

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, 61145 on other resources

Documentation

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