CZ-6A DEB, 61471

Orbit data source: Space-Track

CZ-6A DEB, 61471 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/61471?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61471, 2024-140AAD

Orbit

LEO

Last TLE update

9 hours ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2024-08-06 (9 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 9 hours ago

0 CZ-6A DEB
1 61471U 24140AAD 25114.99934662  .00006203  00000-0  33926-2 0  9997
2 61471  88.9142 319.6978 0113110  97.1764 264.2295 14.08630945 32912

Epoch: 2025-04-24T23:59Z

Definitive object data (Epoch: 2025-04-24T23:59:03.547Z)

Latitude

-0.00011°

Longitude

106.67029°

Altitude

876.251 km

Speed

7.409 km/s

True Right ascension

21h 18m 47s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-12.91661°

Longitude

-73.12943°

Altitude

878.443 km

Speed

7.408 km/s

Apparent Right ascension

07h 28m 14s

Apparent Declination

-29° 55' 43"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

16:38:38

Azimuth

272.741° WNW

Elevation

-54.192°

Doppler factor

Orbital elements

Apogee altitude

942.91 km

Perigee altitude

779.146 km

Semi-major axis

7,239.165 km

Eccentricity

0.011311

Inclination

88.9142°

RAAN

319.6978°

Arg. of periapsis

97.1764°

True anomaly

262.94186°

Mean anomaly

264.2295°

Eccentric anomaly

263.58548°

Mean motion

3.52379 °/min

BSTAR

0.0033926

Orbital period

102.16 mins

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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.
10 mins	2025-04-25 13:43:30.641Z	164.036° S	2025-04-25 13:48:30.641Z	95.437° ESE	41.027°	2025-04-25 13:53:30.641Z	7.539° NNE
4 mins	2025-04-25 15:29:30.641Z	259.592° W	2025-04-25 15:31:30.641Z	284.367° WNW	14.633°	2025-04-25 15:33:30.641Z	308.538° NW
9 mins	2025-04-26 02:08:30.641Z	352.401° N	2025-04-26 02:12:30.641Z	274.468° WNW	42.416°	2025-04-26 02:17:30.641Z	193.478° SSW

Authenticating...

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Check out CZ-6A DEB, 61471 on other resources

View CZ-6A DEB, 61471 on Heavens-Above

View CZ-6A DEB, 61471 on Keep Track

View CZ-6A DEB, 61471 on Celestrak

View CZ-6A DEB, 61471 on Gunter's Space Page

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