CZ-4C R/B, 48341

Orbit data source: Space-Track

CZ-4C R/B, 48341 is space debris in LEO originally from a launch on Fri, 30 Apr 2021 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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/48341?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

48341, 2021-037B

Orbit

LEO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

CZ-4 STAGE 3, Unknown motor

Mass

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

Launch date (UTC)

2021-04-30 (5 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 2.5 m

Radar Cross Section

14.536 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago

0 CZ-4C R/B
1 48341U 21037B   26171.28225972 -.00000066  00000-0  31241-4 0  9995
2 48341  63.4465  23.2946 0234215   8.0427 352.4259 13.59769189255206

Epoch: 2026-06-20T06:46Z

TLE epoch observation values (Epoch: 2026-06-20T06:46:27.239Z)

Latitude

-0.00004°

Longitude

13.18197°

Altitude

866.223 km

Speed

7.505 km/s

True Right ascension

01h 33m 10s

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

21:27:31

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,208.98 km

Perigee altitude

861.71 km

Semi-major axis

7,413.482 km

Eccentricity

0.02342

Inclination

63.4465°

RAAN

23.2946°

Arg. of periapsis

8.0427°

True anomaly

352.06158°

Mean anomaly

352.4259°

Eccentric anomaly

352.24482°

Mean motion

3.40024 °/min

Orbital period

105.87 mins

BSTAR

0.000031241

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Other satellites on launch #37 in the year 2021 (2021-04-30 UTC)

YAOGAN-34, 48340

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CZ-4C 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.
11 mins	2026-06-22 15:22:31.199Z	201.493° SSW	2026-06-22 15:27:31.199Z	130.814° SE	43.073°	2026-06-22 15:33:31.199Z	38.465° NE
7 mins	2026-06-22 17:14:31.199Z	281.888° WNW	2026-06-22 17:17:31.199Z	320.907° NNW	22.113°	2026-06-22 17:21:31.199Z	7.765° NNE
12 mins	2026-06-22 22:48:31.199Z	342.839° N	2026-06-22 22:54:31.199Z	45.828° ENE	26.774°	2026-06-22 23:00:31.199Z	101.871° ESE
13 mins	2026-06-23 00:38:31.199Z	318.928° NNW	2026-06-23 00:44:31.199Z	222.759° SW	42.396°	2026-06-23 00:51:31.199Z	160.248° 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-4C R/B, 48341 on other resources

View CZ-4C R/B, 48341 on Heavens-Above

View CZ-4C R/B, 48341 on Keep Track

View CZ-4C R/B, 48341 on Celestrak

View CZ-4C R/B, 48341 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-4C R/B, 48341

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-06-20T06:46:27.239Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #37 in the year 2021 (2021-04-30 UTC)

CZ-4C R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4C R/B, 48341 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago