TJS-23, 67226
Orbit data source: Space-Track
TJS-23, 67226 is a Chinese payload satellite in GEO that was launched on Sat, 20 Dec 2025 UTC via a CHANG ZHENG 5 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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67226 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational Defense Sigint
Bus & Motor
TJS11, Unknown motor
Mass
~10,000 kg wet, ~6,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan + 1 Dish, 1.1 m
Radar Cross Section
63.841 m²
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 TJS-23
1 67226U 25306A 26099.78899722 .00000014 00000-0 00000+0 0 9991
2 67226 5.7443 297.8280 0006834 120.5485 239.3395 1.00277903 1206Epoch: 2026-04-09T18:56Z
TLE epoch observation values (Epoch: 2026-04-09T18:56:09.359Z)
Latitude
-0°
Longitude
175.58591°
Altitude
35,798.99 km
Speed
3.074 km/s
True Right ascension
19h 50m 37s
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
02:26:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,814.75 km
Perigee altitude
35,757.12 km
Semi-major axis
42,164.072 km
Eccentricity
0.00068
Inclination
5.7443°
RAAN
297.828°
Arg. of periapsis
120.5485°
True anomaly
239.27217°
Mean anomaly
239.3395°
Eccentric anomaly
239.30583°
Mean motion
0.25069 °/min
Orbital period
1,436.06 mins
BSTAR
0
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Other satellites on launch #306 in the year 2025 (2025-12-20 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.TJS-23 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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| TJS-23 is likely not visible in the next few days. |
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67226 neighbors
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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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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