CZ-6A DEB, 61479

Orbit data source: Space-Track

CZ-6A DEB, 61479 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/61479?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61479, 2024-140AAM

Orbit

LEO

Last TLE update

17 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 17 hours ago

0 CZ-6A DEB
1 61479U 24140AAM 25122.91523974  .00001516  00000-0  86102-3 0  9993
2 61479  89.0697 323.8698 0165193  58.7836 302.9415 14.02789702 35674

Epoch: 2025-05-02T21:57Z

Definitive object data (Epoch: 2025-05-02T21:57:56.713Z)

Latitude

0.00002°

Longitude

133.31849°

Altitude

823.345 km

Speed

7.474 km/s

True Right ascension

21h 35m 28s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-60.76982°

Longitude

-45.09789°

Altitude

1,027.347 km

Speed

7.276 km/s

Apparent Right ascension

10h 02m 05s

Apparent Declination

-51° 02' 32"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

22:17:05

Azimuth

168.025° S

Elevation

-78.572°

Doppler factor

Orbital elements

Apogee altitude

1,001.043 km

Perigee altitude

761.207 km

Semi-major axis

7,259.262 km

Eccentricity

0.0165193

Inclination

89.0697°

RAAN

323.8698°

Arg. of periapsis

58.7836°

True anomaly

301.33505°

Mean anomaly

302.9415°

Eccentric anomaly

302.14006°

Mean motion

3.50917 °/min

BSTAR

0.00086102

Orbital period

102.59 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.
4 mins	2025-05-03 15:14:35.092Z	257.624° W	2025-05-03 15:16:35.092Z	282.303° WNW	13.463°	2025-05-03 15:18:35.092Z	306.958° NW
5 mins	2025-05-04 00:15:35.092Z	58.182° ENE	2025-05-04 00:17:35.092Z	82.436° E	15.06°	2025-05-04 00:20:35.092Z	114.494° SE
9 mins	2025-05-04 01:56:35.092Z	350.402° N	2025-05-04 02:00:35.092Z	257.225° W	41.852°	2025-05-04 02:05:35.092Z	194.889° SSW
8 mins	2025-05-04 13:27:35.092Z	162.96° S	2025-05-04 13:31:35.092Z	79.897° E	41.673°	2025-05-04 13:35:35.092Z	7.836° NNE

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Check out CZ-6A DEB, 61479 on other resources

View CZ-6A DEB, 61479 on Heavens-Above

View CZ-6A DEB, 61479 on Keep Track

View CZ-6A DEB, 61479 on Celestrak

View CZ-6A DEB, 61479 on Gunter's Space Page

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