CZ-4B DEB, 57397

Orbit data source: Space-Track

CZ-4B DEB, 57397 is space debris in SSO originally from a launch on Wed, 24 Oct 2018 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/57397?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

57397, 2018-081Q

Orbit

SSO

Last TLE update

4 days ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2018-10-24 (7 years 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 4 days ago

0 CZ-4B DEB
1 57397U 18081Q   25125.45761349  .00002402  00000-0  64441-3 0  9993
2 57397  99.3902  10.0878 0198691 346.9461  12.6623 14.38226768108350

Epoch: 2025-05-05T10:58Z

Definitive object data (Epoch: 2025-05-05T10:58:57.805Z)

Latitude

-0.00002°

Longitude

-18.22394°

Altitude

628.93 km

Speed

7.617 km/s

True Right ascension

00h 40m 21s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

24.38834°

Longitude

-18.31284°

Altitude

672.378 km

Speed

7.573 km/s

Apparent Right ascension

01h 42m 03s

Apparent Declination

-6° 13' 32"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

15:04:13

Azimuth

34.154° NE

Elevation

-51.588°

Doppler factor

Orbital elements

Apogee altitude

903.389 km

Perigee altitude

619.671 km

Semi-major axis

7,139.667 km

Eccentricity

0.0198691

Inclination

99.3902°

RAAN

10.0878°

Arg. of periapsis

346.9461°

True anomaly

13.17377°

Mean anomaly

12.6623°

Eccentric anomaly

12.91678°

Mean motion

3.59771 °/min

BSTAR

0.00064441

Orbital period

100.06 mins

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Other satellites on launch #81 in the year 2018 (2018-10-24 UTC)

HAIYANG 2B, 43655

CZ-4B R/B, 43656

CZ-4B DEB, 43659 (Decayed)

CZ-4B DEB, 43660

CZ-4B DEB, 43661

CZ-4B DEB, 56085 (Decayed)

CZ-4B DEB, 56086 (Decayed)

CZ-4B DEB, 56087 (Decayed)

CZ-4B DEB, 56088

CZ-4B DEB, 56089 (Decayed)

CZ-4B DEB, 56090 (Decayed)

CZ-4B DEB, 56160 (Decayed)

CZ-4B DEB, 56161 (Decayed)

CZ-4B DEB, 57396 (Decayed)

CZ-4B 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	2025-05-09 15:18:18.986Z	115.375° SE	2025-05-09 15:21:18.986Z	69.488° E	23.439°	2025-05-09 15:25:18.986Z	11.327° NNE
7 mins	2025-05-09 16:57:18.986Z	208.343° SW	2025-05-09 17:00:18.986Z	263.955° W	27.694°	2025-05-09 17:04:18.986Z	324.069° NNW
9 mins	2025-05-10 05:06:18.986Z	21.437° NNE	2025-05-10 05:10:18.986Z	132.031° SE	43.674°	2025-05-10 05:15:18.986Z	188.687° SSW
5 mins	2025-05-10 06:46:18.986Z	322.828° NNW	2025-05-10 06:48:18.986Z	298.334° NW	16.632°	2025-05-10 06:51:18.986Z	264.828° W

Authenticating...

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Check out CZ-4B DEB, 57397 on other resources

View CZ-4B DEB, 57397 on Heavens-Above

View CZ-4B DEB, 57397 on Keep Track

View CZ-4B DEB, 57397 on Celestrak

View CZ-4B DEB, 57397 on Gunter's Space Page

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