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, 2.9 m
Radar Cross Section
14.536 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   26286.63728196  .00000631  00000-0  10192-3 0  9994
2 41728  97.9475 350.0881 0097794 170.1394 190.1763 14.71729800545551
Epoch: 2026-10-13T15:17Z
TLE epoch observation values (Epoch: 2026-10-13T15:17:41.161Z)
Latitude
-0.00001°
Longitude
98.4681°
Altitude
726.299 km
Speed
7.456 km/s
True Right ascension
23h 20m 21s
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
19:39:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
721.361 km
Perigee altitude
583.848 km
Semi-major axis
7,030.742 km
Eccentricity
0.00978
Inclination
97.9475°
RAAN
350.0881°
Arg. of periapsis
170.1394°
True anomaly
189.98066°
Mean anomaly
190.1763°
Eccentric anomaly
190.07825°
Mean motion
3.68164 °/min
Orbital period
97.78 mins
BSTAR
0.00010192
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Other satellites on launch #49 in the year 2016 (2016-08-09 UTC)

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