BEIDOU IGSO-6, 41434
Orbit data source: Space-Track
BEIDOU IGSO-6, 41434 is a payload satellite owned by CNSA (CN) that was launched on Tue, 29 Mar 2016 UTC via a CHANG ZHENG 3A 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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41434 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational Defense Navigation
Bus & Motor
DFH-3, FY-25
Mass
2,300 kg wet, 1,300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 9.0 m
Radar Cross Section
13.998 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 BEIDOU IGSO-6
1 41434U 16021A 26282.86302916 -.00000180 00000-0 00000-0 0 9991
2 41434 60.3916 36.9079 0062932 228.9668 159.9751 1.00277195 38639Epoch: 2026-10-09T20:42Z
TLE epoch observation values (Epoch: 2026-10-09T20:42:45.719Z)
Latitude
25.15514°
Longitude
83.15634°
Altitude
36,035.169 km
Speed
3.057 km/s
True Right ascension
03h 29m 18s
True Declination
25° 07' 59"
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
03:33:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,050.305 km
Perigee altitude
35,519.624 km
Semi-major axis
42,163.101 km
Eccentricity
0.00629
Inclination
60.3916°
RAAN
36.9079°
Arg. of periapsis
228.9668°
True anomaly
160.22023°
Mean anomaly
159.9751°
Eccentric anomaly
160.09784°
Mean motion
0.25069 °/min
Orbital period
1,436.01 mins
BSTAR
0
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Other satellites on launch #21 in the year 2016 (2016-03-29 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 IGSO-6 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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| BEIDOU IGSO-6 is likely not visible in the next few days. |
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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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 descending order |
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