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

Last TLE update

4 days ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2024-08-06 (11 months ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 4 days ago

0 CZ-6A DEB
1 61472U 24140AAE 25186.80877985  .00002015  00000-0  15885-2 0  9992
2 61472  89.0518 317.9589 0228086 293.9645  63.7790 13.80022991 42091

Epoch: 2025-07-05T19:24Z

TLE epoch observation values (Epoch: 2025-07-05T19:24:38.579Z)

Latitude

0.00004°

Longitude

102.75665°

Altitude

895.92 km

Speed

7.44 km/s

True Right ascension

21h 11m 50s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

88.25378°

Longitude

-110.31752°

Altitude

1,141.91 km

Speed

7.207 km/s

Apparent Right ascension

14h 21m 31s

Apparent Declination

35° 25' 41"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

02:31:36

Azimuth

2.121° NNE

Elevation

-14.62°

Doppler factor

Orbital elements

Apogee altitude

1,128.203 km

Perigee altitude

793.42 km

Semi-major axis

7,338.948 km

Eccentricity

0.02281

Inclination

89.0518°

RAAN

317.9589°

Arg. of periapsis

293.9645°

True anomaly

Unknown

Mean anomaly

63.779°

Eccentric anomaly

Unknown

Mean motion

3.45217 °/min

Orbital period

104.28 mins

BSTAR

0.0015885

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

CZ-6A DEB, 61470 (Decayed)

CZ-6A DEB Visibility forecast

Observer location: undefined°, undefined°

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.
11 mins	2025-07-09 19:42:58.301Z	23.174° NE	2025-07-09 19:48:58.301Z	85.469° E	25.754°	2025-07-09 19:53:58.301Z	137.024° SSE
11 mins	2025-07-09 21:27:58.301Z	345.026° N	2025-07-09 21:32:58.301Z	282.391° WNW	36.395°	2025-07-09 21:38:58.301Z	208.509° SW
6 mins	2025-07-10 07:27:58.301Z	99.592° ESE	2025-07-10 07:30:58.301Z	66.919° ENE	17.506°	2025-07-10 07:33:58.301Z	37.659° NE
11 mins	2025-07-10 09:08:58.301Z	188.669° SSW	2025-07-10 09:13:58.301Z	269.153° W	43.351°	2025-07-10 09:19:58.301Z	353.749° N

Authenticating...

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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

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