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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Edit Public Description
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: 10 hours ago
TLE from 10 hours ago
0 XINGCHI-1 02A
1 58496U 23187A 25247.25229152 .00003233 00000-0 40522-3 0 9998
2 58496 97.9504 326.8236 0011806 3.9301 356.2003 14.82876244 94727Epoch: 2025-09-04T06:03Z
TLE epoch observation values (Epoch: 2025-09-04T06:03:17.987Z)
Latitude
-0.00001°
Longitude
-107.61884°
Altitude
615.038 km
Speed
7.556 km/s
True Right ascension
21h 47m 17s
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
08:26:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
625.558 km
Perigee altitude
609.04 km
Semi-major axis
6,995.436 km
Eccentricity
0.00118
Inclination
97.9504°
RAAN
326.8236°
Arg. of periapsis
3.9301°
True anomaly
356.19132°
Mean anomaly
356.2003°
Eccentric anomaly
356.19581°
Mean motion
3.70955 °/min
Orbital period
97.05 mins
BSTAR
0.00040522
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Other satellites on launch #187 in the year 2023 (2023-12-04 UTC)
XINGCHI-1 02A Visibility forecast
Observer location: undefined°, undefined°
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-04 17:57:46.441Z | 24.624° NE | 2025-09-04 18:01:46.441Z | 126.893° SE | 38.029° | 2025-09-04 18:04:46.441Z | 175.704° S |
| 6 mins | 2025-09-05 04:52:46.441Z | 125.512° SE | 2025-09-05 04:54:46.441Z | 77.389° E | 31.936° | 2025-09-05 04:58:46.441Z | 4.101° NNE |
| 4 mins | 2025-09-05 06:29:46.441Z | 243.544° WSW | 2025-09-05 06:30:46.441Z | 259.865° W | 16.006° | 2025-09-05 06:33:46.441Z | 305.836° NW |
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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Authenticating...
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