CZ-4B R/B, 61938

Orbit data source: Space-Track

CZ-4B R/B, 61938 is space debris in SSO originally from a launch on Wed, 13 Nov 2024 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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Iframe URL

https://www.satcat.com/sats-embedded/61938?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61938, 2024-208C

Orbit

SSO

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)

2024-11-13 (2 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 2.5 m

Radar Cross Section

14.536 m², Large (>1 m²)

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Last TLE update: 14 hours ago

TLE from 14 hours ago

0 CZ-4B R/B
1 61938U 24208C   26150.10596122  .00009027  00000-0  25964-3 0  9990
2 61938  97.9441 200.0264 0124941 226.6417 132.4359 15.28543812 85511

Epoch: 2026-05-30T02:32Z

TLE epoch observation values (Epoch: 2026-05-30T02:32:35.049Z)

Latitude

-0.00008°

Longitude

-85.74638°

Altitude

541.659 km

Speed

7.559 km/s

True Right ascension

13h 20m 06s

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

01:45:53

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

562.793 km

Perigee altitude

391.492 km

Semi-major axis

6,855.279 km

Eccentricity

0.01249

Inclination

97.9441°

RAAN

200.0264°

Arg. of periapsis

226.6417°

True anomaly

133.48147°

Mean anomaly

132.4359°

Eccentric anomaly

132.95979°

Mean motion

3.82389 °/min

Orbital period

94.14 mins

BSTAR

0.00025964

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Other satellites on launch #208 in the year 2024 (2024-11-13 UTC)

HAIYANG 4A, 61936

OBJECT B, 61937

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CZ-4B 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.
6 mins	2026-05-31 03:48:36.492Z	197.323° SSW	2026-05-31 03:51:36.492Z	270.658° WNW	32.572°	2026-05-31 03:54:36.492Z	328.536° 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 R/B, 61938 on other resources

View CZ-4B R/B, 61938 on Heavens-Above

View CZ-4B R/B, 61938 on Keep Track

View CZ-4B R/B, 61938 on Celestrak

View CZ-4B R/B, 61938 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 R/B, 61938

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 14 hours ago

TLE from 14 hours ago

TLE epoch observation values (Epoch: 2026-05-30T02:32:35.049Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #208 in the year 2024 (2024-11-13 UTC)

CZ-4B R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4B R/B, 61938 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 14 hours ago