XIAOXIANG 2, 43155 (Decayed)
Orbit data source: Space-Track
XIAOXIANG 2, 43155 was a payload satellite owned by Changsha Tianyi (CN) 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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43155 intel report (Beta)
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XIAOXIANG 2 radio frequencies
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changsha Tianyi
Mission
Decayed Commercial Communications
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
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 XIAOXIANG 2
1 43155U 18008A 24235.75891043 .18791616 24620-5 29649-3 0 9999
2 43155 97.1927 292.6688 0013149 268.0079 91.9719 16.47546330365397Epoch: 2024-08-22T18:12Z
TLE epoch observation values (Epoch: 2024-08-22T18:12:49.861Z)
Latitude
-0.00002°
Longitude
47.91892°
Altitude
149.379 km
Speed
7.816 km/s
True Right ascension
19h 30m 40s
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
04:35:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
151.168 km
Perigee altitude
134.019 km
Semi-major axis
6,520.73 km
Eccentricity
0.00131
Inclination
97.1927°
RAAN
292.6688°
Arg. of periapsis
268.0079°
True anomaly
92.12248°
Mean anomaly
91.9719°
Eccentric anomaly
92.04719°
Mean motion
4.12191 °/min
Orbital period
87.34 mins
BSTAR
0.00029649
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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.XIAOXIANG 2 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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