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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Identifier
41728, 2016-049B
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
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 (10 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)

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

TLE from 2 days ago
0 CZ-4C R/B
1 41728U 16049B   26171.46135069  .00000480  00000-0  79727-4 0  9991
2 41728  97.9605 237.4628 0097787 178.4561 181.6967 14.71621154528614
Epoch: 2026-06-20T11:04Z
TLE epoch observation values (Epoch: 2026-06-20T11:04:20.699Z)
Latitude
-0.00005°
Longitude
162.70092°
Altitude
727.675 km
Speed
7.455 km/s
True Right ascension
15h 49m 51s
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
21:36:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
721.707 km
Perigee altitude
584.197 km
Semi-major axis
7,031.089 km
Eccentricity
0.00978
Inclination
97.9605°
RAAN
237.4628°
Arg. of periapsis
178.4561°
True anomaly
181.66392°
Mean anomaly
181.6967°
Eccentric anomaly
181.68027°
Mean motion
3.68137 °/min
Orbital period
97.79 mins
BSTAR
0.000079727
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Other satellites on launch #49 in the year 2016 (2016-08-09 UTC)

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