CZ-2D R/B, 43486

Orbit data source: Space-Track

CZ-2D R/B, 43486 is space debris in SSO originally from a launch on Sat, 02 Jun 2018 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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
43486, 2018-048C
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
Unknown
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
2018-06-02 (8 years ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cone, 0.1 m
Radar Cross Section
0.025 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 CZ-2D R/B
1 43486U 18048C   26196.04208561  .00002289  00000-0  21015-3 0  9999
2 43486  97.5744 224.8294 0012808  71.1866 289.0744 14.95744689439324
Epoch: 2026-07-15T01:00Z
TLE epoch observation values (Epoch: 2026-07-15T01:00:36.196Z)
Latitude
0.00001°
Longitude
-83.225°
Altitude
580.212 km
Speed
7.572 km/s
True Right ascension
14h 59m 19s
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
03:41:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.976 km
Perigee altitude
568.16 km
Semi-major axis
6,955.205 km
Eccentricity
0.00128
Inclination
97.5744°
RAAN
224.8294°
Arg. of periapsis
71.1866°
True anomaly
288.93562°
Mean anomaly
289.0744°
Eccentric anomaly
289.00502°
Mean motion
3.74178 °/min
Orbital period
96.21 mins
BSTAR
0.00021015
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Other satellites on launch #48 in the year 2018 (2018-06-02 UTC)

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