TIANXING-1 02, 58756 (Decayed)
Orbit data source: Space-Track
TIANXING-1 02, 58756 was a payload satellite owned by CAS IOM (CN) in LEO that was launched on Thu, 11 Jan 2024 UTC via a KUAIZHOU-1A 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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58756 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAS IOM
Mission
Decayed Civil Science
Bus & Motor
TIANXING, Unknown motor
Mass
200 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 1.5 m
Radar Cross Section
0.900 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months ago
0 TIANXING-1 02
1 58756U 24008A 25259.37537501 .09101139 13006-5 72685-3 0 9999
2 58756 95.0994 178.3423 0008908 200.5406 159.5543 16.40065956 95883Epoch: 2025-09-16T09:00Z
TLE epoch observation values (Epoch: 2025-09-16T09:00:32.400Z)
Latitude
0.00001°
Longitude
47.64072°
Altitude
174.401 km
Speed
7.798 km/s
True Right ascension
11h 53m 22s
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
21:28:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
168.173 km
Perigee altitude
156.521 km
Semi-major axis
6,540.484 km
Eccentricity
0.00089
Inclination
95.0994°
RAAN
178.3423°
Arg. of periapsis
200.5406°
True anomaly
159.58992°
Mean anomaly
159.5543°
Eccentric anomaly
159.57211°
Mean motion
4.10325 °/min
Orbital period
87.74 mins
BSTAR
0.00072685
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Other satellites on launch #8 in the year 2024 (2024-01-11 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.TIANXING-1 02 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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