CZ-6A DEB, 61472

Orbit data source: Space-Track

CZ-6A DEB, 61472 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/61472?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61472, 2024-140AAE

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: 1 day ago

TLE from 1 day ago

0 CZ-6A DEB
1 61472U 24140AAE 26113.93786099  .00001290  00000-0  97902-3 0  9997
2 61472  89.0347 288.2352 0232180 124.8812 237.4424 13.81306690 82402

Epoch: 2026-04-23T22:30Z

TLE epoch observation values (Epoch: 2026-04-23T22:30:31.189Z)

Latitude

-0.00003°

Longitude

98.62748°

Altitude

1,056.713 km

Speed

7.276 km/s

True Right ascension

19h 12m 56s

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

12:36:21

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,126.55 km

Perigee altitude

785.97 km

Semi-major axis

7,334.397 km

Eccentricity

0.02322

Inclination

89.0347°

RAAN

288.2352°

Arg. of periapsis

124.8812°

True anomaly

235.23497°

Mean anomaly

237.4424°

Eccentric anomaly

236.3352°

Mean motion

3.45539 °/min

Orbital period

104.19 mins

BSTAR

0.00097902

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

QIANFAN-4, 60382

QIANFAN-5, 60383

CZ-6A DEB, 61433 (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.
10 mins	2026-04-25 11:07:50.311Z	142.792° SSE	2026-04-25 11:12:50.311Z	84.028° E	29.65°	2026-04-25 11:17:50.311Z	19.13° NNE
9 mins	2026-04-25 12:52:50.311Z	220.897° SW	2026-04-25 12:56:50.311Z	270.354° WNW	27.067°	2026-04-25 13:01:50.311Z	335.515° NNW
9 mins	2026-04-25 23:46:50.311Z	2.441° NNE	2026-04-25 23:50:50.311Z	58.66° ENE	44.894°	2026-04-25 23:55:50.311Z	180.665° 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, 61472 on other resources

View CZ-6A DEB, 61472 on Heavens-Above

View CZ-6A DEB, 61472 on Keep Track

View CZ-6A DEB, 61472 on Celestrak

View CZ-6A DEB, 61472 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, 61472

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: 2026-04-23T22:30:31.189Z)

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, 61472 on other resources

Documentation

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