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

14 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 14 hours ago

0 CZ-6A DEB
1 61476U 24140AAJ 25123.05882959  .00000371  00000-0  20714-3 0  9992
2 61476  88.9884 321.2124 0109227  91.7294 269.6403 14.05658425 33847

Epoch: 2025-05-03T01:24Z

Definitive object data (Epoch: 2025-05-03T01:24:42.876Z)

Latitude

0.00004°

Longitude

78.82722°

Altitude

878.663 km

Speed

7.412 km/s

True Right ascension

21h 24m 50s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

60.65207°

Longitude

-103.02924°

Altitude

815.589 km

Speed

7.487 km/s

Apparent Right ascension

10h 31m 44s

Apparent Declination

15° 00' 37"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

23:24:54

Azimuth

15.477° NNE

Elevation

-33.696°

Doppler factor

Orbital elements

Apogee altitude

950.421 km

Perigee altitude

792.055 km

Semi-major axis

7,249.375 km

Eccentricity

0.0109227

Inclination

88.9884°

RAAN

321.2124°

Arg. of periapsis

91.7294°

True anomaly

268.38888°

Mean anomaly

269.6403°

Eccentric anomaly

269.01457°

Mean motion

3.51635 °/min

BSTAR

0.00020714

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.
6 mins	2025-05-04 00:13:12.837Z	42.246° NE	2025-05-04 00:16:12.837Z	79.399° E	17.249°	2025-05-04 00:19:12.837Z	116.321° SE
9 mins	2025-05-04 01:55:12.837Z	344.971° N	2025-05-04 01:59:12.837Z	264.998° W	37.838°	2025-05-04 02:04:12.837Z	201.248° SSW
9 mins	2025-05-04 13:24:12.837Z	170.324° S	2025-05-04 13:28:12.837Z	128.31° SE	43.423°	2025-05-04 13:33:12.837Z	3.29° NNE

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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