XINGCHI-1 02A, 58496
Orbit data source: Space-Track
XINGCHI-1 02A, 58496 is a payload satellite owned by Tuoyuan Shikong (CN) in SSO that was launched on Mon, 04 Dec 2023 UTC via a CHANG ZHENG 2C 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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58496 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Weina
Mission
Operational Commercial Imaging
Bus & Motor
MN35, Unknown motor
Mass
35 kg wet, 35 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.195 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 XINGCHI-1 02A
1 58496U 23187A 26172.51983194 .00001020 00000-0 12797-3 0 9993
2 58496 97.9267 255.3433 0012741 127.2877 232.9501 14.84279417137761Epoch: 2026-06-21T12:28Z
TLE epoch observation values (Epoch: 2026-06-21T12:28:33.479Z)
Latitude
-0.00001°
Longitude
158.48488°
Altitude
624.252 km
Speed
7.544 km/s
True Right ascension
17h 01m 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
14:24:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
621.792 km
Perigee altitude
603.978 km
Semi-major axis
6,991.022 km
Eccentricity
0.00127
Inclination
97.9267°
RAAN
255.3433°
Arg. of periapsis
127.2877°
True anomaly
232.83369°
Mean anomaly
232.9501°
Eccentric anomaly
232.89188°
Mean motion
3.71306 °/min
Orbital period
96.96 mins
BSTAR
0.00012797
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Other satellites on launch #187 in the year 2023 (2023-12-04 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.XINGCHI-1 02A Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-22 04:47:37.189Z | 124.75° SE | 2026-06-22 04:50:37.189Z | 75.609° E | 24.796° | 2026-06-22 04:53:37.189Z | 18.579° NNE |
| 5 mins | 2026-06-22 06:24:37.189Z | 223.472° SW | 2026-06-22 06:26:37.189Z | 259.899° W | 21.936° | 2026-06-22 06:29:37.189Z | 312.698° NW |
| 7 mins | 2026-06-22 18:10:37.189Z | 24.864° NE | 2026-06-22 18:13:37.189Z | 97.013° ESE | 40.358° | 2026-06-22 18:17:37.189Z | 179.921° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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