CZ-6A DEB, 55887

Orbit data source: Space-Track

CZ-6A DEB, 55887 is space debris in SSO originally from a launch on Fri, 11 Nov 2022 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/55887?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

55887, 2022-151AAK

Orbit

SSO

Last TLE update

1 day ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2022-11-11 (3 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 1 day ago

0 CZ-6A DEB
1 55887U 22151AAK 25132.52000298  .00006548  00000-0  26803-2 0  9997
2 55887  98.8060 146.3631 0055086  48.2643 312.3228 14.26694118123910

Epoch: 2025-05-12T12:28Z

Definitive object data (Epoch: 2025-05-12T12:28:48.257Z)

Latitude

-0.00005°

Longitude

88.63012°

Altitude

779.204 km

Speed

7.478 km/s

True Right ascension

09h 45m 27s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-55.22432°

Longitude

102.64002°

Altitude

831.356 km

Speed

7.432 km/s

Apparent Right ascension

12h 05m 48s

Apparent Declination

-49° 30' 11"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

01:16:14

Azimuth

133.445° SE

Elevation

-74.301°

Doppler factor

Orbital elements

Apogee altitude

839.498 km

Perigee altitude

760.415 km

Semi-major axis

7,178.094 km

Eccentricity

0.0055086

Inclination

98.806°

RAAN

146.3631°

Arg. of periapsis

48.2643°

True anomaly

311.85392°

Mean anomaly

312.3228°

Eccentric anomaly

312.08858°

Mean motion

3.56886 °/min

BSTAR

0.0026803

Orbital period

100.87 mins

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Other satellites on launch #151 in the year 2022 (2022-11-11 UTC)

CZ-6A DEB, 55885 (Decayed)

CZ-6A DEB, 55886

CZ-6A DEB, 55888

CZ-6A DEB, 55889 (Decayed)

CZ-6A DEB, 55890 (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	2025-05-13 23:57:55.475Z	121.909° SE	2025-05-14 00:01:55.475Z	61.586° ENE	25.648°	2025-05-14 00:05:55.475Z	8.816° NNE
7 mins	2025-05-14 01:37:55.475Z	208.118° SW	2025-05-14 01:40:55.475Z	254.284° W	27.249°	2025-05-14 01:44:55.475Z	319.839° NNW
8 mins	2025-05-14 13:52:55.475Z	12.054° NNE	2025-05-14 13:55:55.475Z	351.9° N	44.481°	2025-05-14 14:00:55.475Z	197.157° SSW

Authenticating...

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Check out CZ-6A DEB, 55887 on other resources

View CZ-6A DEB, 55887 on Heavens-Above

View CZ-6A DEB, 55887 on Keep Track

View CZ-6A DEB, 55887 on Celestrak

View CZ-6A DEB, 55887 on Gunter's Space Page

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