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 (7 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, Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 CZ-2D R/B
1 43486U 18048C   25260.05929700  .00004329  00000-0  42595-3 0  9999
2 43486  97.6102 293.8224 0011462   2.3821 357.7451 14.92548911394374
Epoch: 2025-09-17T01:25Z
TLE epoch observation values (Epoch: 2025-09-17T01:25:23.26Z)
Latitude
-0.00006°
Longitude
-83.76519°
Altitude
585.056 km
Speed
7.572 km/s
True Right ascension
19h 35m 17s
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
23:56:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.986 km
Perigee altitude
579.019 km
Semi-major axis
6,965.139 km
Eccentricity
0.00115
Inclination
97.6102°
RAAN
293.8224°
Arg. of periapsis
2.3821°
True anomaly
357.73992°
Mean anomaly
357.7451°
Eccentric anomaly
357.74251°
Mean motion
3.73378 °/min
Orbital period
96.42 mins
BSTAR
0.00042595
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Other satellites on launch #48 in the year 2018 (2018-06-02 UTC)

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