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

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 (11 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 61478U 24140AAL 25189.62194866  .00084633  00000-0  43903-2 0  9999
2 61478  89.0643 312.5890 0048618 293.6051  66.0091 15.14755378 45646

Epoch: 2025-07-08T14:55Z

TLE epoch observation values (Epoch: 2025-07-08T14:55:36.364Z)

Latitude

0.00007°

Longitude

161.87319°

Altitude

511.403 km

Speed

7.616 km/s

True Right ascension

20h 50m 21s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

-5.7623°

Longitude

161.65716°

Altitude

510.804 km

Speed

7.616 km/s

Apparent Right ascension

18h 28m 01s

Apparent Declination

-29° 20' 51"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

02:51:39

Azimuth

266.123° W

Elevation

-44.96°

Doppler factor

Orbital elements

Apogee altitude

552.068 km

Perigee altitude

485.007 km

Semi-major axis

6,896.675 km

Eccentricity

0.00486

Inclination

89.0643°

RAAN

312.589°

Arg. of periapsis

293.6051°

True anomaly

Unknown

Mean anomaly

66.0091°

Eccentric anomaly

Unknown

Mean motion

3.78951 °/min

Orbital period

95 mins

BSTAR

0.0043903

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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	2025-07-09 20:01:58.675Z	22.906° NE	2025-07-09 20:04:58.675Z	85.455° E	30.799°	2025-07-09 20:07:58.675Z	150.226° SSE
6 mins	2025-07-10 08:16:58.675Z	152.048° SSE	2025-07-10 08:18:58.675Z	105.078° ESE	36.104°	2025-07-10 08:22:58.675Z	10.875° NNE

Authenticating...

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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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