CZ-3B R/B, 44796

Orbit data source: Space-Track

CZ-3B R/B, 44796 is space debris in HEO originally from a launch on Sat, 23 Nov 2019 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 URL

https://www.satcat.com/sats-embedded/44796?theme=dark&initialShowStats=false

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Identifier

44796, 2019-078D

Orbit

HEO

Country

CN / PRC

Related business

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

Manufacturer

CALT

Mission

Spacecraft

Bus & Motor

CZ-3A STAGE 3, Unknown motor

Mass

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

Launch date (UTC)

2019-11-23 (6 years 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: 1 day ago

TLE from 1 day ago

0 CZ-3B R/B
1 44796U 19078D   26085.17415930  .00000314  00000-0  40007-3 0  9998
2 44796  54.9455  79.3242 5395938 236.5006  60.1962  4.81610854109455

Epoch: 2026-03-26T04:10Z

TLE epoch observation values (Epoch: 2026-03-26T04:10:47.363Z)

Latitude

-0.00002°

Longitude

-167.01562°

Altitude

8,581.645 km

Speed

5.137 km/s

True Right ascension

05h 17m 14s

True Declination

0° 00' 00"

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

14:24:12

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

16,425.809 km

Perigee altitude

441.245 km

Semi-major axis

14,811.664 km

Eccentricity

0.53959

Inclination

54.9455°

RAAN

79.3242°

Arg. of periapsis

236.5006°

True anomaly

123.58308°

Mean anomaly

60.1962°

Eccentric anomaly

91.10688°

Mean motion

1.20403 °/min

Orbital period

299 mins

BSTAR

0.00040007

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Other satellites on launch #78 in the year 2019 (2019-11-23 UTC)

BEIDOU 3M21, 44793

YZ-1 R/B, 44795

BEIDOU 3M22, 44794

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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.
36 mins	2026-03-27 13:12:25.459Z	314.373° NW	2026-03-27 13:36:25.459Z	291.185° WNW	14.278°	2026-03-27 13:48:25.459Z	265.084° W
132 mins	2026-03-27 20:26:25.459Z	94.6° ESE	2026-03-27 21:33:25.459Z	63.618° ENE	20.134°	2026-03-27 22:38:25.459Z	41.101° NE
217 mins	2026-03-28 00:53:25.459Z	206.695° SW	2026-03-28 02:32:25.459Z	300.513° NW	44.954°	2026-03-28 04:30:25.459Z	62.777° ENE
117 mins	2026-03-28 07:08:25.459Z	293.159° NW	2026-03-28 09:05:25.459Z	313.726° NW	38.525°	2026-03-28 09:05:25.459Z	313.726° NW

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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, 44796 on other resources

View CZ-3B R/B, 44796 on Heavens-Above

View CZ-3B R/B, 44796 on Keep Track

View CZ-3B R/B, 44796 on Celestrak

View CZ-3B R/B, 44796 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, 44796

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: 2026-03-26T04:10:47.363Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #78 in the year 2019 (2019-11-23 UTC)

CZ-3B R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-3B R/B, 44796 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 day ago