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: 15 hours ago

TLE from 15 hours ago
0 CZ-2D R/B
1 43486U 18048C   26316.03020013  .00004589  00000-0  40900-3 0  9995
2 43486  97.5635 340.8559 0011680  33.2404 326.9549 14.96430034457264
Epoch: 2026-11-12T00:43Z
TLE epoch observation values (Epoch: 2026-11-12T00:43:29.291Z)
Latitude
-0.00004°
Longitude
-81.18569°
Altitude
574.182 km
Speed
7.577 km/s
True Right ascension
22h 43m 25s
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
12:05:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.063 km
Perigee altitude
566.82 km
Semi-major axis
6,953.079 km
Eccentricity
0.00117
Inclination
97.5635°
RAAN
340.8559°
Arg. of periapsis
33.2404°
True anomaly
326.88183°
Mean anomaly
326.9549°
Eccentric anomaly
326.91837°
Mean motion
3.7435 °/min
Orbital period
96.17 mins
BSTAR
0.000409
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Other satellites on launch #48 in the year 2018 (2018-06-02 UTC)

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