XIAOXIANG 1, 41842 (Decayed)
Orbit data source: Space-Track
XIAOXIANG 1, 41842 was a payload satellite owned by Changsha Tianyi (CN) in LEO that was launched on Wed, 09 Nov 2016 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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41842 intel report (Beta)
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XIAOXIANG 1 radio frequencies
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changsha Tianyi
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
8 kg wet, 8 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.105 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 XIAOXIANG 1
1 41842U 16066B 24239.82917430 .15290837 25672-5 14151-3 0 9999
2 41842 97.3077 273.1412 0013464 246.9911 112.9975 16.50962723435203Epoch: 2024-08-26T19:54Z
TLE epoch observation values (Epoch: 2024-08-26T19:54:00.659Z)
Latitude
-0°
Longitude
-0.91552°
Altitude
143.508 km
Speed
7.818 km/s
True Right ascension
18h 12m 33s
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
07:11:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
142.358 km
Perigee altitude
124.823 km
Semi-major axis
6,511.728 km
Eccentricity
0.00135
Inclination
97.3077°
RAAN
273.1412°
Arg. of periapsis
246.9911°
True anomaly
113.13943°
Mean anomaly
112.9975°
Eccentric anomaly
113.06847°
Mean motion
4.13046 °/min
Orbital period
87.16 mins
BSTAR
0.00014151
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Other satellites on launch #66 in the year 2016 (2016-11-09 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.XIAOXIANG 1 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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