SUPERVIEW-1 01, 41907 (Decayed)
Orbit data source: Space-Track
SUPERVIEW-1 01, 41907 was a payload satellite owned by Beijing HSJ (CN) in LEO that was launched on Wed, 28 Dec 2016 UTC via a CHANG ZHENG 2D launch vehicle from the Taiyaun Space Center, China (TSC). 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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41907 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Decayed Commercial Imaging
Bus & Motor
CAST3000B, Unknown motor
Mass
~600 kg wet, ~560 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.0 m
Radar Cross Section
5.141 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 SUPERVIEW-1 01
1 41907U 16083A 25015.25502111 .16941719 25348-5 27070-3 0 9993
2 41907 97.3950 127.6411 0011795 303.8607 115.5181 16.47619838446894Epoch: 2025-01-15T06:07Z
TLE epoch observation values (Epoch: 2025-01-15T06:07:13.823Z)
Latitude
58.80844°
Longitude
-91.42308°
Altitude
158.963 km
Speed
7.815 km/s
True Right ascension
07h 41m 20s
True Declination
58° 38' 31"
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
08:14:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
150.099 km
Perigee altitude
134.717 km
Semi-major axis
6,520.545 km
Eccentricity
0.00118
Inclination
97.395°
RAAN
127.6411°
Arg. of periapsis
303.8607°
True anomaly
115.64°
Mean anomaly
115.5181°
Eccentric anomaly
115.57906°
Mean motion
4.12209 °/min
Orbital period
87.33 mins
BSTAR
0.0002707
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Other satellites on launch #83 in the year 2016 (2016-12-28 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.SUPERVIEW-1 01 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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