CZ-6A DEB, 61476

Orbit data source: Space-Track

CZ-6A DEB, 61476 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/61476?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61476, 2024-140AAJ

Orbit

LEO

Last TLE update

12 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 12 hours ago

0 CZ-6A DEB
1 61476U 24140AAJ 25114.87243574  .00000370  00000-0  20646-3 0  9999
2 61476  88.9892 322.1303 0109506 117.0413 244.1996 14.05652262 32690

Epoch: 2025-04-24T20:56Z

Definitive object data (Epoch: 2025-04-24T20:56:18.447Z)

Latitude

-0.00008°

Longitude

154.9158°

Altitude

912.595 km

Speed

7.378 km/s

True Right ascension

21h 28m 31s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

65.74944°

Longitude

-27.37519°

Altitude

806.322 km

Speed

7.497 km/s

Apparent Right ascension

06h 20m 40s

Apparent Declination

20° 35' 31"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

16:40:11

Azimuth

333.967° NNW

Elevation

-25.112°

Doppler factor

Orbital elements

Apogee altitude

950.645 km

Perigee altitude

791.874 km

Semi-major axis

7,249.396 km

Eccentricity

0.0109506

Inclination

88.9892°

RAAN

322.1303°

Arg. of periapsis

117.0413°

True anomaly

243.07661°

Mean anomaly

244.1996°

Eccentric anomaly

243.63743°

Mean motion

3.51634 °/min

BSTAR

0.00020646

Orbital period

102.38 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 14:08:03.939Z	174.371° S	2025-04-25 14:13:03.939Z	31.705° NE	44.446°	2025-04-25 14:18:03.939Z	0.746° NNE
6 mins	2025-04-26 00:53:03.939Z	46.761° ENE	2025-04-26 00:55:03.939Z	73.102° E	18.054°	2025-04-26 00:59:03.939Z	123.571° SE
8 mins	2025-04-26 02:35:03.939Z	338.95° N	2025-04-26 02:38:03.939Z	281.048° WNW	35.793°	2025-04-26 02:43:03.939Z	205.311° SW

Authenticating...

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Check out CZ-6A DEB, 61476 on other resources

View CZ-6A DEB, 61476 on Heavens-Above

View CZ-6A DEB, 61476 on Keep Track

View CZ-6A DEB, 61476 on Celestrak

View CZ-6A DEB, 61476 on Gunter's Space Page

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