CZ-6A DEB, 61427

Orbit data source: Space-Track

CZ-6A DEB, 61427 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/61427?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

61427, 2024-140YU

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 (1 year 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: 21 hours ago

TLE from 21 hours ago

0 CZ-6A DEB
1 61427U 24140YU  25341.25439496  .00477365  00000-0  89411-2 0  9995
2 61427  88.7884 277.3893 0049645  84.3430 276.3487 15.45711272 70564

Epoch: 2025-12-07T06:06Z

TLE epoch observation values (Epoch: 2025-12-07T06:06:19.724Z)

Latitude

-0.00008°

Longitude

109.5367°

Altitude

428.947 km

Speed

7.656 km/s

True Right ascension

18h 29m 33s

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

01:09:37

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

459.843 km

Perigee altitude

392.284 km

Semi-major axis

6,804.201 km

Eccentricity

0.00496

Inclination

88.7884°

RAAN

277.3893°

Arg. of periapsis

84.343°

True anomaly

275.78292°

Mean anomaly

276.3487°

Eccentric anomaly

276.06585°

Mean motion

3.86703 °/min

Orbital period

93.09 mins

BSTAR

0.0089411

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

CZ-6A DEB, 61298 (Decayed)

CZ-6A DEB, 61378 (Decayed)

CZ-6A DEB, 61337 (Decayed)

CZ-6A DEB, 61415

CZ-6A DEB, 61143

CZ-6A DEB, 61418

CZ-6A DEB, 60900

CZ-6A DEB, 61796

CZ-6A DEB, 60778

CZ-6A DEB, 60668

CZ-6A DEB, 60621

CZ-6A DEB, 60896

CZ-6A DEB, 61087

CZ-6A DEB, 60716

CZ-6A DEB, 61101

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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.
4 mins	2025-12-08 07:31:34.353Z	43.345° NE	2025-12-08 07:33:34.353Z	89.785° E	18.443°	2025-12-08 07:35:34.353Z	131.173° SE

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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, 61427 on other resources

View CZ-6A DEB, 61427 on Heavens-Above

View CZ-6A DEB, 61427 on Keep Track

View CZ-6A DEB, 61427 on Celestrak

View CZ-6A DEB, 61427 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

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