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 (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: 12 hours ago

TLE from 12 hours ago
0 CZ-4C R/B
1 41728U 16049B   25296.14346367  .00001331  00000-0  20907-3 0  9999
2 41728  97.9932   1.9672 0097511 226.6091 132.6966 14.71176487493271
Epoch: 2025-10-23T03:26Z
TLE epoch observation values (Epoch: 2025-10-23T03:26:35.261Z)
Latitude
-0.00006°
Longitude
-81.48666°
Altitude
707.21 km
Speed
7.477 km/s
True Right ascension
00h 07m 52s
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
10:57:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
722.946 km
Perigee altitude
585.797 km
Semi-major axis
7,032.508 km
Eccentricity
0.00975
Inclination
97.9932°
RAAN
1.9672°
Arg. of periapsis
226.6091°
True anomaly
133.51107°
Mean anomaly
132.6966°
Eccentric anomaly
133.10451°
Mean motion
3.68025 °/min
Orbital period
97.82 mins
BSTAR
0.00020907
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Other satellites on launch #49 in the year 2016 (2016-08-09 UTC)

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