CZ-6A DEB, 61472

Orbit data source: Space-Track

CZ-6A DEB, 61472 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/61472?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61472, 2024-140AAE

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 61472U 24140AAE 25114.00579722  .00001990  00000-0  15588-2 0  9994
2 61472  89.0541 325.2959 0233291 155.2235 206.0355 13.79750741 32052

Epoch: 2025-04-24T00:08Z

Definitive object data (Epoch: 2025-04-24T00:08:20.879Z)

Latitude

0.00003°

Longitude

110.92547°

Altitude

1,122.468 km

Speed

7.214 km/s

True Right ascension

21h 41m 11s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

29.03718°

Longitude

111.30898°

Altitude

1,056.378 km

Speed

7.282 km/s

Apparent Right ascension

00h 28m 46s

Apparent Declination

-3° 49' 13"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

16:35:21

Azimuth

73.93° E

Elevation

-23.966°

Doppler factor

Orbital elements

Apogee altitude

1,133.011 km

Perigee altitude

790.544 km

Semi-major axis

7,339.914 km

Eccentricity

0.0233291

Inclination

89.0541°

RAAN

325.2959°

Arg. of periapsis

155.2235°

True anomaly

204.89217°

Mean anomaly

206.0355°

Eccentric anomaly

205.46088°

Mean motion

3.45149 °/min

BSTAR

0.0015588

Orbital period

104.3 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	2025-04-25 12:51:14.149Z	102.387° ESE	2025-04-25 12:54:14.149Z	72.43° E	15.3°	2025-04-25 12:57:14.149Z	42.249° NE
11 mins	2025-04-25 14:32:14.149Z	183.785° SSW	2025-04-25 14:38:14.149Z	312.957° NW	43.727°	2025-04-25 14:43:14.149Z	355.351° N
8 mins	2025-04-26 01:29:14.149Z	29.354° NE	2025-04-26 01:32:14.149Z	73.816° E	27.48°	2025-04-26 01:37:14.149Z	146.334° SSE
6 mins	2025-04-26 03:14:14.149Z	322.449° NNW	2025-04-26 03:17:14.149Z	274.104° WNW	23.694°	2025-04-26 03:20:14.149Z	232.501° WSW

Authenticating...

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Check out CZ-6A DEB, 61472 on other resources

View CZ-6A DEB, 61472 on Heavens-Above

View CZ-6A DEB, 61472 on Keep Track

View CZ-6A DEB, 61472 on Celestrak

View CZ-6A DEB, 61472 on Gunter's Space Page

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