CZ-4B DEB, 46484

Orbit data source: Space-Track

CZ-4B DEB, 46484 is space debris in SSO originally from a launch on Sun, 27 Sep 2020 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/46484?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

46484, 2020-067G

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2020-09-27 (5 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago

0 CZ-4B DEB
1 46484U 20067G   26002.13602827  .00010302  00000-0  89797-3 0  9999
2 46484  97.6480  59.8090 0035347 230.4202 129.3897 14.96580688285108

Epoch: 2026-01-02T03:15Z

TLE epoch observation values (Epoch: 2026-01-02T03:15:52.842Z)

Latitude

0.00002°

Longitude

-90.94176°

Altitude

596.179 km

Speed

7.553 km/s

True Right ascension

03h 59m 14s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

10:23:08

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

599.054 km

Perigee altitude

549.903 km

Semi-major axis

6,952.615 km

Eccentricity

0.00353

Inclination

97.648°

RAAN

59.809°

Arg. of periapsis

230.4202°

True anomaly

129.70186°

Mean anomaly

129.3897°

Eccentric anomaly

129.54587°

Mean motion

3.74387 °/min

Orbital period

96.16 mins

BSTAR

0.00089797

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Other satellites on launch #67 in the year 2020 (2020-09-27 UTC)

CZ-4B R/B, 46481 (Decayed)

CZ-4B DEB, 46482 (Decayed)

CZ-4B DEB, 46483 (Decayed)

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CZ-4B DEB 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.
7 mins	2026-01-02 16:40:17.030Z	8.606° NNE	2026-01-02 16:43:17.030Z	329.901° NNW	43.749°	2026-01-02 16:47:17.030Z	198.166° SSW
6 mins	2026-01-03 03:28:17.030Z	148.673° SSE	2026-01-03 03:31:17.030Z	60.543° ENE	40.272°	2026-01-03 03:34:17.030Z	358.814° N

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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-4B DEB, 46484 on other resources

View CZ-4B DEB, 46484 on Heavens-Above

View CZ-4B DEB, 46484 on Keep Track

View CZ-4B DEB, 46484 on Celestrak

View CZ-4B DEB, 46484 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-4B DEB, 46484

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 7 hours ago

TLE from 7 hours ago

TLE epoch observation values (Epoch: 2026-01-02T03:15:52.842Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #67 in the year 2020 (2020-09-27 UTC)

CZ-4B DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4B DEB, 46484 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 7 hours ago