CZ-6A DEB, 61478

Orbit data source: Space-Track

CZ-6A DEB, 61478 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/61478?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61478, 2024-140AAL

Orbit

LEO

Last TLE update

2 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 2 hours ago

0 CZ-6A DEB
1 61478U 24140AAL 25123.55898532  .00125994  00000-0  90563-2 0  9990
2 61478  89.0780 320.6138 0065381 184.0989 175.9721 15.01961459 35680

Epoch: 2025-05-03T13:24Z

Definitive object data (Epoch: 2025-05-03T13:24:56.331Z)

Latitude

0.00001°

Longitude

-102.32042°

Altitude

609.286 km

Speed

7.53 km/s

True Right ascension

21h 22m 27s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

33.26884°

Longitude

-101.7274°

Altitude

604.799 km

Speed

7.539 km/s

Apparent Right ascension

17h 44m 32s

Apparent Declination

-6° 23' 04"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

22:56:25

Azimuth

257.346° W

Elevation

5.022°

Doppler factor

Orbital elements

Apogee altitude

603.03 km

Perigee altitude

512.336 km

Semi-major axis

6,935.82 km

Eccentricity

0.0065381

Inclination

89.078°

RAAN

320.6138°

Arg. of periapsis

184.0989°

True anomaly

176.0243°

Mean anomaly

175.9721°

Eccentric anomaly

175.99824°

Mean motion

3.75748 °/min

BSTAR

0.0090563

Orbital period

95.81 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 01:10:48.507Z	13.574° NNE	2025-05-04 01:13:48.507Z	80.081° E	38.442°	2025-05-04 01:16:48.507Z	162.949° S
7 mins	2025-05-04 13:31:48.507Z	177.704° S	2025-05-04 13:34:48.507Z	0.134° NNE	44.845°	2025-05-04 13:38:48.507Z	359.023° N

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Check out CZ-6A DEB, 61478 on other resources

View CZ-6A DEB, 61478 on Heavens-Above

View CZ-6A DEB, 61478 on Keep Track

View CZ-6A DEB, 61478 on Celestrak

View CZ-6A DEB, 61478 on Gunter's Space Page

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