DECAYED

CZ-4B DEB, 56086 (Decayed)

Orbit data source: Space-Track

CZ-4B DEB, 56086 was 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 src="https://www.satcat.com/sats-embedded/56086?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/56086?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

56086, 2018-081G

Orbit

Decayed

Last TLE update

4 months ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

Unknown

Mission

Decayed 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 months ago

0 CZ-4B DEB
1 56086U 18081G   25005.17745783  .11139710  43404+0  72806-1 0  9998
2 56086  99.3608 256.2788 0008302 145.7303 214.4499 15.88015211 34266

Epoch: 2025-01-05T04:15Z

Definitive object data (Epoch: 2025-01-05T04:15:32.356Z)

Latitude

-0.00008°

Longitude

87.37693°

Altitude

315.545 km

Speed

7.716 km/s

True Right ascension

17h 05m 06s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization observer readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

310.369 km

Perigee altitude

299.273 km

Semi-major axis

6,682.958 km

Eccentricity

0.0008302

Inclination

99.3608°

RAAN

256.2788°

Arg. of periapsis

145.7303°

True anomaly

214.39613°

Mean anomaly

214.4499°

Eccentric anomaly

214.42301°

Mean motion

3.97274 °/min

BSTAR

0.072806

Orbital period

90.62 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, 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, 57397

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 07:07:34.730Z	62.663° ENE	2025-05-09 07:13:34.730Z	344.786° N	36.653°	2025-05-09 07:14:34.730Z	70.068° E
7 mins	2025-05-10 02:38:34.730Z	5.992° NNE	2025-05-10 02:38:34.730Z	5.992° NNE	42.422°	2025-05-10 02:45:34.730Z	200.949° SSW

Authenticating...

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Check out CZ-4B DEB, 56086 (Decayed) on other resources

View CZ-4B DEB, 56086 (Decayed) on Celestrak

View CZ-4B DEB, 56086 (Decayed) on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.