CZ-3C R/B, 41870

Orbit data source: Space-Track

CZ-3C R/B, 41870 is space debris in HEO originally from a launch on Tue, 22 Nov 2016 UTC launched from the Xichang Space Center, China (XSC). 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
41870, 2016-072B
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2016-11-22 (10 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)

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

TLE from 2 days ago
0 CZ-3C R/B
1 41870U 16072B   26171.00704153  .00000236  00000-0  40317-3 0  9992
2 41870  16.8153 138.0953 5127030  34.0615 350.1508  5.17386993160484
Epoch: 2026-06-20T00:10Z
TLE epoch observation values (Epoch: 2026-06-20T00:10:08.388Z)
Latitude
-0.00003°
Longitude
-132.69719°
Altitude
930.015 km
Speed
8.992 km/s
True Right ascension
09h 12m 15s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
21:26:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
14,988.917 km
Perigee altitude
504.973 km
Semi-major axis
14,125.082 km
Eccentricity
0.5127
Inclination
16.8153°
RAAN
138.0953°
Arg. of periapsis
34.0615°
True anomaly
325.81511°
Mean anomaly
350.1508°
Eccentric anomaly
340.20025°
Mean motion
1.29288 °/min
Orbital period
278.45 mins
BSTAR
0.00040317
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Other satellites on launch #72 in the year 2016 (2016-11-22 UTC)

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