CZ-6A DEB, 61479

Orbit data source: Space-Track

CZ-6A DEB, 61479 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/61479?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61479, 2024-140AAM

Orbit

LEO

Last TLE update

1 day 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 1 day ago

0 CZ-6A DEB
1 61479U 24140AAM 25114.07014762  .00001501  00000-0  85234-3 0  9990
2 61479  89.0706 324.7781 0165455  86.3844 275.6241 14.02759119 34430

Epoch: 2025-04-24T01:41Z

Definitive object data (Epoch: 2025-04-24T01:41:00.754Z)

Latitude

-0.00002°

Longitude

87.1781°

Altitude

877.482 km

Speed

7.418 km/s

True Right ascension

21h 39m 06s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-15.18145°

Longitude

-92.70649°

Altitude

935.287 km

Speed

7.36 km/s

Apparent Right ascension

07h 40m 48s

Apparent Declination

-31° 59' 48"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

16:38:38

Azimuth

267.609° W

Elevation

-52.708°

Doppler factor

Orbital elements

Apogee altitude

1,001.341 km

Perigee altitude

761.121 km

Semi-major axis

7,259.368 km

Eccentricity

0.0165455

Inclination

89.0706°

RAAN

324.7781°

Arg. of periapsis

86.3844°

True anomaly

273.73376°

Mean anomaly

275.6241°

Eccentric anomaly

274.67927°

Mean motion

3.50909 °/min

BSTAR

0.00085234

Orbital period

102.59 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.
9 mins	2025-04-25 13:44:30.806Z	150.213° SSE	2025-04-25 13:49:30.806Z	80.398° E	32.479°	2025-04-25 13:53:30.806Z	18.242° NNE
6 mins	2025-04-25 15:29:30.806Z	240.443° WSW	2025-04-25 15:32:30.806Z	283.745° WNW	20.257°	2025-04-25 15:35:30.806Z	323.232° NNW
9 mins	2025-04-26 02:12:30.806Z	2.772° NNE	2025-04-26 02:16:30.806Z	166.473° S	44.144°	2025-04-26 02:21:30.806Z	181.086° SSW

Authenticating...

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Check out CZ-6A DEB, 61479 on other resources

View CZ-6A DEB, 61479 on Heavens-Above

View CZ-6A DEB, 61479 on Keep Track

View CZ-6A DEB, 61479 on Celestrak

View CZ-6A DEB, 61479 on Gunter's Space Page

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