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: 1 day ago

TLE from 1 day ago

0 CZ-4B DEB
1 49046U 20067H   26271.34735973  .00001080  00000-0  15778-3 0  9997
2 49046  97.7311 304.0929 0028208 322.8997  37.0263 14.77444023299119

Epoch: 2026-09-28T08:20Z

TLE epoch observation values (Epoch: 2026-09-28T08:20:11.880Z)

Latitude

-0.0001°

Longitude

171.91539°

Altitude

624.645 km

Speed

7.555 km/s

True Right ascension

20h 16m 22s

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

09:22:20

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

654.222 km

Perigee altitude

614.659 km

Semi-major axis

7,012.578 km

Eccentricity

0.00282

Inclination

97.7311°

RAAN

304.0929°

Arg. of periapsis

322.8997°

True anomaly

37.2215°

Mean anomaly

37.0263°

Eccentric anomaly

37.12384°

Mean motion

3.69595 °/min

Orbital period

97.4 mins

BSTAR

0.00015778

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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, 46484

HJ-2A, 46478

HJ-2B, 46479

CZ-4B DEB, 46480 (Decayed)

CZ-4B DEB, 46483 (Decayed)

CZ-4B DEB, 46482 (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.
5 mins	2026-09-29 15:49:07.349Z	326.32° NNW	2026-09-29 15:50:07.349Z	301.308° NW	35.567°	2026-09-29 15:54:07.349Z	225.879° WSW
6 mins	2026-09-30 02:44:07.349Z	198.333° SSW	2026-09-30 02:46:07.349Z	246.079° WSW	46.519°	2026-09-30 02:50:07.349Z	333.145° NNW
6 mins	2026-09-30 14:34:07.349Z	42.705° NE	2026-09-30 14:37:07.349Z	108.339° ESE	34.315°	2026-09-30 14:40:07.349Z	158.411° S

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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

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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: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-09-28T08:20:11.880Z)

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: 1 day ago