DECAYED

CZ-3B R/B, 62189 (Decayed)

Orbit data source: Space-Track

CZ-3B R/B, 62189 was space debris originally from a launch on Tue, 03 Dec 2024 UTC launched from the Xichang Space Center, China (XSC). 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/62189?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/62189?theme=dark&initialShowStats=false

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Identifier

62189, 2024-227B

Orbit

Decayed

Country

CN / PRC

Related business

China Aerospace Science and Technology Corporation (CASC) (CN)

Manufacturer

CALT

Mission

Decayed spacecraft

Bus & Motor

CZ-3A STAGE 3, Unknown motor

Mass

~2,800 kg wet, ~2,800 kg dry

Launch date (UTC)

2024-12-03 (1 year ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + 1 Nozzle, 6.2 m

Radar Cross Section

32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 months ago

TLE from 10 months ago

0 CZ-3B R/B
1 62189U 24227B   25052.03828810 -.00001123  71063-5  00000+0 0  9996
2 62189  51.1975  84.9873 3177569 246.9654  81.8039  9.34586791  1663

Epoch: 2025-02-21T00:55Z

TLE epoch observation values (Epoch: 2025-02-21T00:55:08.091Z)

Latitude

3.45266°

Longitude

-77.23162°

Altitude

3,654.199 km

Speed

6.133 km/s

True Right ascension

05h 51m 01s

True Declination

3° 26' 17"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

16:23:35

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

6,168.086 km

Perigee altitude

117.427 km

Semi-major axis

9,520.894 km

Eccentricity

0.31776

Inclination

51.1975°

RAAN

84.9873°

Arg. of periapsis

246.9654°

True anomaly

117.52877°

Mean anomaly

81.8039°

Eccentric anomaly

99.74721°

Mean motion

2.33629 °/min

Orbital period

154.09 mins

BSTAR

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Computing Atmospheric mass density...

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Other satellites on launch #227 in the year 2024 (2024-12-03 UTC)

TJS-13, 62188

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CZ-3B R/B Visibility forecast

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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.
21 mins	2026-01-01 16:57:41.674Z	238.589° WSW	2026-01-01 17:02:41.674Z	316.652° NNW	44.734°	2026-01-01 17:18:41.674Z	55.814° ENE
37 mins	2026-01-01 19:39:41.674Z	294.79° NW	2026-01-01 19:48:41.674Z	11.814° NNE	39.461°	2026-01-01 20:16:41.674Z	82.867° E
57 mins	2026-01-01 22:20:41.674Z	305.164° NW	2026-01-01 22:37:41.674Z	40.081° NE	44.713°	2026-01-01 23:17:41.674Z	127.302° SE
59 mins	2026-01-02 01:03:41.674Z	301.314° NW	2026-01-02 01:26:41.674Z	236.944° WSW	38.375°	2026-01-02 02:02:41.674Z	173.513° S
21 mins	2026-01-02 03:59:41.674Z	275.619° WNW	2026-01-02 04:09:41.674Z	259.35° W	12.456°	2026-01-02 04:20:41.674Z	242.791° WSW
15 mins	2026-01-02 16:04:41.674Z	204.453° SW	2026-01-02 16:07:41.674Z	110.779° ESE	42.017°	2026-01-02 16:19:41.674Z	54.775° ENE

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out CZ-3B R/B, 62189 (Decayed) on other resources

View CZ-3B R/B, 62189 (Decayed) on Celestrak

View CZ-3B R/B, 62189 (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.

CZ-3B R/B, 62189 (Decayed)

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 months ago

TLE from 10 months ago

TLE epoch observation values (Epoch: 2025-02-21T00:55:08.091Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #227 in the year 2024 (2024-12-03 UTC)

CZ-3B R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-3B R/B, 62189 (Decayed) on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 months ago