CZ-6A DEB, 61468

Orbit data source: Space-Track

CZ-6A DEB, 61468 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/61468?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61468, 2024-140AAA

Orbit

LEO

Last TLE update

20 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 20 hours ago

0 CZ-6A DEB
1 61468U 24140AAA 25114.58005584  .00154778  00000-0  11055-1 0  9999
2 61468  89.2118 326.1622 0083164 157.7504 202.7374 15.01021695 34506

Epoch: 2025-04-24T13:55Z

Definitive object data (Epoch: 2025-04-24T13:55:16.824Z)

Latitude

-0.00011°

Longitude

-95.50735°

Altitude

620.242 km

Speed

7.52 km/s

True Right ascension

21h 44m 38s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

70.38045°

Longitude

-93.39036°

Altitude

569.219 km

Speed

7.586 km/s

Apparent Right ascension

02h 50m 40s

Apparent Declination

26° 12' 20"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

16:40:11

Azimuth

25.896° NE

Elevation

-19.13°

Doppler factor

Orbital elements

Apogee altitude

618.284 km

Perigee altitude

502.874 km

Semi-major axis

6,938.716 km

Eccentricity

0.0083164

Inclination

89.2118°

RAAN

326.1622°

Arg. of periapsis

157.7504°

True anomaly

202.37256°

Mean anomaly

202.7374°

Eccentric anomaly

202.55463°

Mean motion

3.75513 °/min

BSTAR

0.011055

Orbital period

95.87 mins

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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, 61469

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.
7 mins	2025-04-25 14:02:03.760Z	154.893° SSE	2025-04-25 14:06:03.760Z	80.311° E	34.142°	2025-04-25 14:09:03.760Z	17.477° NNE
5 mins	2025-04-26 01:42:03.760Z	38.51° NE	2025-04-26 01:44:03.760Z	81.735° E	23.363°	2025-04-26 01:47:03.760Z	140.847° SSE

Authenticating...

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Check out CZ-6A DEB, 61468 on other resources

View CZ-6A DEB, 61468 on Heavens-Above

View CZ-6A DEB, 61468 on Keep Track

View CZ-6A DEB, 61468 on Celestrak

View CZ-6A DEB, 61468 on Gunter's Space Page

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