CHUANG XIN 26 (CX-26), 69972
Orbit data source: Space-Track
CHUANG XIN 26 (CX-26), 69972 is a payload satellite owned by CNSA (CN) in LEO that was launched on Fri, 10 Jul 2026 UTC via a CHANG ZHENG 10B launch vehicle from the Wenchang Satellite Launch Center (WSC). 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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69972 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
~10,000 kg wet, ~10,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CHUANG XIN 26 (CX-26)
1 69972U 26158A 26192.48090097 -.00000088 00000-0 30360-4 0 9995
2 69972 49.9853 296.0945 0004897 288.4346 71.6034 14.25145244 172Epoch: 2026-07-11T11:32Z
TLE epoch observation values (Epoch: 2026-07-11T11:32:29.843Z)
Latitude
-0.00009°
Longitude
-166.42343°
Altitude
807.424 km
Speed
7.451 km/s
True Right ascension
19h 44m 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
06:52:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
812.265 km
Perigee altitude
805.226 km
Semi-major axis
7,186.882 km
Eccentricity
0.00049
Inclination
49.9853°
RAAN
296.0945°
Arg. of periapsis
288.4346°
True anomaly
71.65666°
Mean anomaly
71.6034°
Eccentric anomaly
71.63003°
Mean motion
3.56232 °/min
Orbital period
101.06 mins
BSTAR
0.00003036
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Other satellites on launch #158 in the year 2026 (2026-07-10 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.CHUANG XIN 26 (CX-26) 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-07-13 09:09:05.343Z | 215.533° SW | 2026-07-13 09:13:05.343Z | 152.236° SSE | 40.819° | 2026-07-13 09:18:05.343Z | 62.806° ENE |
| 9 mins | 2026-07-13 10:55:05.343Z | 272.147° WNW | 2026-07-13 10:59:05.343Z | 333.873° NNW | 34.332° | 2026-07-13 11:04:05.343Z | 48.45° ENE |
| 7 mins | 2026-07-13 12:43:05.343Z | 314.863° NW | 2026-07-13 12:46:05.343Z | 1.323° NNE | 25.806° | 2026-07-13 12:50:05.343Z | 55.193° ENE |
| 9 mins | 2026-07-13 14:29:05.343Z | 317.428° NNW | 2026-07-13 14:33:05.343Z | 30.464° NE | 34.72° | 2026-07-13 14:38:05.343Z | 94.093° ESE |
| 9 mins | 2026-07-13 16:15:05.343Z | 292.549° NW | 2026-07-13 16:19:05.343Z | 202.545° SW | 39.86° | 2026-07-13 16:24:05.343Z | 143.095° SSE |
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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