CZ-6A DEB, 61469

Orbit data source: Space-Track

CZ-6A DEB, 61469 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/61469?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61469, 2024-140AAB

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 (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 17 hours ago

0 CZ-6A DEB
1 61469U 24140AAB 25189.90285668  .00003444  00000-0  49027-3 0  9996
2 61469  90.0423 354.2815 0136180 288.9429  69.7070 14.70466505 47070

Epoch: 2025-07-08T21:40Z

TLE epoch observation values (Epoch: 2025-07-08T21:40:06.817Z)

Latitude

-0.00007°

Longitude

102.16192°

Altitude

630.617 km

Speed

7.56 km/s

True Right ascension

23h 37m 07s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

18.8169°

Longitude

-77.82004°

Altitude

716.632 km

Speed

7.47 km/s

Apparent Right ascension

12h 59m 44s

Apparent Declination

-9° 38' 09"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

02:55:19

Azimuth

48.236° ENE

Elevation

-50.301°

Doppler factor

Orbital elements

Apogee altitude

752.252 km

Perigee altitude

560.658 km

Semi-major axis

7,034.592 km

Eccentricity

0.01362

Inclination

90.0423°

RAAN

354.2815°

Arg. of periapsis

288.9429°

True anomaly

Unknown

Mean anomaly

69.707°

Eccentric anomaly

Unknown

Mean motion

3.67862 °/min

Orbital period

97.86 mins

BSTAR

0.00049027

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Other satellites on launch #140 in the year 2024 (2024-08-06 UTC)

QIANFAN-1, 60379

CZ-6A DEB, 60625

CZ-6A DEB, 61468

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.
8 mins	2025-07-09 22:44:38.153Z	21.395° NNE	2025-07-09 22:48:38.153Z	83.565° E	31.784°	2025-07-09 22:52:38.153Z	151.624° SSE
6 mins	2025-07-10 00:23:38.153Z	322.493° NNW	2025-07-10 00:26:38.153Z	276.947° WNW	20.601°	2025-07-10 00:29:38.153Z	236.854° WSW
8 mins	2025-07-10 11:21:38.153Z	178.518° S	2025-07-10 11:24:38.153Z	208.16° SW	44.783°	2025-07-10 11:29:38.153Z	356.933° N

Authenticating...

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Check out CZ-6A DEB, 61469 on other resources

View CZ-6A DEB, 61469 on Heavens-Above

View CZ-6A DEB, 61469 on Keep Track

View CZ-6A DEB, 61469 on Celestrak

View CZ-6A DEB, 61469 on Gunter's Space Page

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