BEIDOU 3M17, 43706
Orbit data source: Space-Track
BEIDOU 3M17, 43706 is a payload satellite owned by CNSA (CN) in MEO that was launched on Sun, 18 Nov 2018 UTC via a CHANG ZHENG 3B/YZ-1 launch vehicle from the Xichang Space Center, China (XSC). 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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43706 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational Defense Navigation
Bus & Motor
BD-3M/SAR, Unknown motor
Mass
1,014 kg wet, ~850 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 5.0 m
Radar Cross Section
8.984 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 BEIDOU 3M17
1 43706U 18093A 26172.18891355 .00000078 00000-0 00000+0 0 9993
2 43706 54.1692 182.1601 0010176 292.3320 147.9319 1.86228431 51616Epoch: 2026-06-21T04:32Z
TLE epoch observation values (Epoch: 2026-06-21T04:32:02.130Z)
Latitude
53.07114°
Longitude
-81.4712°
Altitude
21,559.821 km
Speed
3.777 km/s
True Right ascension
17h 03m 43s
True Declination
53° 01' 44"
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
21:25:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,556.745 km
Perigee altitude
21,499.95 km
Semi-major axis
27,906.484 km
Eccentricity
0.00102
Inclination
54.1692°
RAAN
182.1601°
Arg. of periapsis
292.332°
True anomaly
147.99374°
Mean anomaly
147.9319°
Eccentric anomaly
147.96283°
Mean motion
0.46557 °/min
Orbital period
773.24 mins
BSTAR
0
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Other satellites on launch #93 in the year 2018 (2018-11-18 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.BEIDOU 3M17 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 302 mins | 2026-06-23 05:21:25.082Z | 253.939° W | 2026-06-23 09:30:25.082Z | 48.281° ENE | 44.604° | 2026-06-23 10:23:25.082Z | 124.829° SE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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