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

2 days ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2022-11-11 (2 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 2 days ago

0 CZ-6A DEB
1 55887U 22151AAK 25113.02113969  .00010568  00000-0  43406-2 0  9996
2 55887  98.8102 126.7463 0056474 102.4493 258.3014 14.26316055121135

Epoch: 2025-04-23T00:30Z

Definitive object data (Epoch: 2025-04-23T00:30:26.469Z)

Latitude

0.00002°

Longitude

-92.1769°

Altitude

815.437 km

Speed

7.441 km/s

True Right ascension

08h 26m 59s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

38.84164°

Longitude

97.30956°

Altitude

780.555 km

Speed

7.482 km/s

Apparent Right ascension

00h 12m 14s

Apparent Declination

3° 28' 29"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

15:57:04

Azimuth

64.106° ENE

Elevation

-22.761°

Doppler factor

Orbital elements

Apogee altitude

841.771 km

Perigee altitude

760.681 km

Semi-major axis

7,179.363 km

Eccentricity

0.0056474

Inclination

98.8102°

RAAN

126.7463°

Arg. of periapsis

102.4493°

True anomaly

257.66862°

Mean anomaly

258.3014°

Eccentric anomaly

257.98492°

Mean motion

3.56791 °/min

BSTAR

0.0043406

Orbital period

100.9 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.
9 mins	2025-04-25 13:41:03.921Z	16.398° NNE	2025-04-25 13:46:03.921Z	136.292° SSE	44.278°	2025-04-25 13:50:03.921Z	189.756° SSW
9 mins	2025-04-26 01:01:03.921Z	175.647° S	2025-04-26 01:05:03.921Z	246.449° WSW	43.003°	2025-04-26 01:10:03.921Z	341.012° N

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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