CZ-4B DEB, 49046

Orbit data source: Space-Track

CZ-4B DEB, 49046 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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https://www.satcat.com/sats-embedded/49046?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

49046, 2020-067H

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 (6 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

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago

0 CZ-4B DEB
1 49046U 20067H   26155.32112919  .00002370  00000-0  34014-3 0  9992
2 49046  97.7382 192.7673 0028676 340.0869  19.9220 14.77116695281983

Epoch: 2026-06-04T07:42Z

TLE epoch observation values (Epoch: 2026-06-04T07:42:25.562Z)

Latitude

-0.00008°

Longitude

-175.60627°

Altitude

622.549 km

Speed

7.558 km/s

True Right ascension

12h 51m 04s

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

13:00:37

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

655.59 km

Perigee altitude

615.365 km

Semi-major axis

7,013.615 km

Eccentricity

0.00287

Inclination

97.7382°

RAAN

192.7673°

Arg. of periapsis

340.0869°

True anomaly

20.03435°

Mean anomaly

19.922°

Eccentric anomaly

19.97814°

Mean motion

3.69514 °/min

Orbital period

97.43 mins

BSTAR

0.00034014

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

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

HJ-2A, 46478

HJ-2B, 46479

CZ-4B DEB, 46482 (Decayed)

CZ-4B DEB, 46480

CZ-4B DEB, 46483 (Decayed)

CZ-4B DEB, 46484

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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.
6 mins	2026-06-07 14:19:58.693Z	50.125° ENE	2026-06-07 14:22:58.693Z	93.939° ESE	17.917°	2026-06-07 14:25:58.693Z	136.984° SSE
6 mins	2026-06-07 15:56:58.693Z	345.036° N	2026-06-07 15:59:58.693Z	273.71° WNW	31.523°	2026-06-07 16:02:58.693Z	224.474° SW
6 mins	2026-06-08 02:52:58.693Z	192.295° SSW	2026-06-08 02:55:58.693Z	277.73° WNW	37.22°	2026-06-08 02:58:58.693Z	332.993° NNW

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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, 49046 on other resources

View CZ-4B DEB, 49046 on Heavens-Above

View CZ-4B DEB, 49046 on Keep Track

View CZ-4B DEB, 49046 on Celestrak

View CZ-4B DEB, 49046 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, 49046

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-06-04T07:42:25.562Z)

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, 49046 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago