CZ-4C R/B, 41728

Orbit data source: Space-Track

CZ-4C R/B, 41728 is space debris in SSO originally from a launch on Tue, 09 Aug 2016 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/41728?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

41728, 2016-049B

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)

2016-08-09 (9 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
Last TLE update: 10 hours ago

TLE from 10 hours ago

0 CZ-4C R/B
1 41728U 16049B   26036.14694838  .00001030  00000-0  16292-3 0  9999
2 41728  97.9777 104.9734 0096781 251.5250 107.5419 14.71432299508719

Epoch: 2026-02-05T03:31Z

TLE epoch observation values (Epoch: 2026-02-05T03:31:36.340Z)

Latitude

-0.00005°

Longitude

-83.23137°

Altitude

680.628 km

Speed

7.505 km/s

True Right ascension

06h 59m 53s

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

15:19:50

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

721.608 km

Perigee altitude

585.501 km

Semi-major axis

7,031.692 km

Eccentricity

0.00968

Inclination

97.9777°

RAAN

104.9734°

Arg. of periapsis

251.525°

True anomaly

108.59545°

Mean anomaly

107.5419°

Eccentric anomaly

108.06907°

Mean motion

3.6809 °/min

Orbital period

97.8 mins

BSTAR

0.00016292

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Other satellites on launch #49 in the year 2016 (2016-08-09 UTC)

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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.
8 mins	2026-02-05 17:09:29.414Z	19.192° NNE	2026-02-05 17:13:29.414Z	87.94° E	42.468°	2026-02-05 17:17:29.414Z	182.781° SSW
8 mins	2026-02-06 04:08:29.414Z	145.711° SSE	2026-02-06 04:11:29.414Z	91.095° ESE	39.162°	2026-02-06 04:16:29.414Z	356.487° N
4 mins	2026-02-06 05:47:29.414Z	248.462° W	2026-02-06 05:48:29.414Z	262.154° W	14.456°	2026-02-06 05:51:29.414Z	301.71° 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-4C R/B, 41728 on other resources

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View CZ-4C R/B, 41728 on Celestrak

View CZ-4C R/B, 41728 on Gunter's Space Page

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CZ-4C R/B, 41728

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 10 hours ago

TLE from 10 hours ago

TLE epoch observation values (Epoch: 2026-02-05T03:31:36.340Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #49 in the year 2016 (2016-08-09 UTC)

CZ-4C R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4C R/B, 41728 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 10 hours ago