XINGCHI-1 02B, 58498
Orbit data source: Space-Track
XINGCHI-1 02B, 58498 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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58498 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 02B
1 58498U 23187C 26172.52763361 .00001039 00000-0 12561-3 0 9997
2 58498 97.9296 256.5958 0011839 122.9889 237.2466 14.85823189137829Epoch: 2026-06-21T12:39Z
TLE epoch observation values (Epoch: 2026-06-21T12:39:47.543Z)
Latitude
-0.00001°
Longitude
156.92109°
Altitude
618.516 km
Speed
7.547 km/s
True Right ascension
17h 06m 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
14:23:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
616.309 km
Perigee altitude
599.767 km
Semi-major axis
6,986.175 km
Eccentricity
0.00118
Inclination
97.9296°
RAAN
256.5958°
Arg. of periapsis
122.9889°
True anomaly
237.1326°
Mean anomaly
237.2466°
Eccentric anomaly
237.18959°
Mean motion
3.71693 °/min
Orbital period
96.85 mins
BSTAR
0.00012561
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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 02B 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 04:57:50.041Z | 127.915° SE | 2026-06-22 05:00:50.041Z | 74.565° E | 27.232° | 2026-06-22 05:03:50.041Z | 15.281° NNE |
| 5 mins | 2026-06-22 06:34:50.041Z | 228.598° WSW | 2026-06-22 06:36:50.041Z | 263.666° W | 19.603° | 2026-06-22 06:39:50.041Z | 312.073° NW |
| 6 mins | 2026-06-22 18:20:50.041Z | 26.101° NE | 2026-06-22 18:22:50.041Z | 84.852° E | 42.142° | 2026-06-22 18:26:50.041Z | 183.348° SSW |
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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