CZ-4C R/B, 44623

Orbit data source: Space-Track

CZ-4C R/B, 44623 is space debris in SSO originally from a launch on Fri, 04 Oct 2019 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/44623?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

44623, 2019-066B

Orbit

SSO

Last TLE update

17 hours ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

CZ-4 STAGE 3, Unknown motor

Mass

~1,000 kg wet, ~1,000 kg dry

Launch date (UTC)

2019-10-04 (6 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 1.4 m

Radar Cross Section

7.676 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 17 hours ago

0 CZ-4C R/B
1 44623U 19066B   25199.78698310  .00044855  00000-0  40588-3 0  9993
2 44623  97.7913 278.3575 0042721 226.7993 132.9695 15.66741688322181

Epoch: 2025-07-18T18:53Z

TLE epoch observation values (Epoch: 2025-07-18T18:53:15.339Z)

Latitude

-0.00005°

Longitude

58.21016°

Altitude

391.091 km

Speed

7.664 km/s

True Right ascension

18h 33m 25s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

61.1382°

Longitude

-106.69591°

Altitude

386.422 km

Speed

7.68 km/s

Apparent Right ascension

10h 59m 09s

Apparent Declination

16° 23' 16"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

01:04:57

Azimuth

34.019° NE

Elevation

-26.532°

Doppler factor

Orbital elements

Apogee altitude

393.963 km

Perigee altitude

336.347 km

Semi-major axis

6,743.292 km

Eccentricity

0.00427

Inclination

97.7913°

RAAN

278.3575°

Arg. of periapsis

226.7993°

True anomaly

133.32641°

Mean anomaly

132.9695°

Eccentric anomaly

133.14808°

Mean motion

3.91954 °/min

Orbital period

91.85 mins

BSTAR

0.00040588

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Other satellites on launch #66 in the year 2019 (2019-10-04 UTC)

GAOFEN 10R, 44622

CZ-4C R/B Visibility forecast

Observer location: undefined°, undefined°

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.
4 mins	2025-07-19 18:26:14.221Z	357.107° N	2025-07-19 18:28:14.221Z	302.345° NW	35.489°	2025-07-19 18:30:14.221Z	217.529° SW

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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Authenticating...

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Check out CZ-4C R/B, 44623 on other resources

View CZ-4C R/B, 44623 on Heavens-Above

View CZ-4C R/B, 44623 on Keep Track

View CZ-4C R/B, 44623 on Celestrak

View CZ-4C R/B, 44623 on Gunter's Space Page

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