ZHOU ENLAI, 43156 (Decayed)
Orbit data source: Space-Track
ZHOU ENLAI, 43156 was a Chinese payload satellite in LEO that was launched on Fri, 19 Jan 2018 UTC via a CHANG ZHENG 11 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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43156 intel report (Beta)
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ZHOU ENLAI radio frequencies
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Ling Zhong
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.025 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 ZHOU ENLAI
1 43156U 18008B 24198.66905212 .17296646 24655-5 28398-3 0 9992
2 43156 97.2151 256.8209 0016593 258.3712 101.5729 16.46899832359648Epoch: 2024-07-16T16:03Z
TLE epoch observation values (Epoch: 2024-07-16T16:03:26.103Z)
Latitude
-0.00004°
Longitude
80.97753°
Altitude
152.968 km
Speed
7.813 km/s
True Right ascension
17h 07m 17s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
10:52:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
155.125 km
Perigee altitude
133.48 km
Semi-major axis
6,522.439 km
Eccentricity
0.00166
Inclination
97.2151°
RAAN
256.8209°
Arg. of periapsis
258.3712°
True anomaly
101.7591°
Mean anomaly
101.5729°
Eccentric anomaly
101.66601°
Mean motion
4.12029 °/min
Orbital period
87.37 mins
BSTAR
0.00028398
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Other satellites on launch #8 in the year 2018 (2018-01-19 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ZHOU ENLAI Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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