YAOGAN 26, 40362
Orbit data source: Space-Track
YAOGAN 26, 40362 is a payload satellite owned by PLA GAD (CN) in SSO that was launched on Sat, 27 Dec 2014 UTC via a CHANG ZHENG 4B launch vehicle from the Taiyaun Space Center, China (TSC). 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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40362 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational Defense Imaging
Bus & Motor
JB-13?, Unknown motor
Mass
~3,000 kg wet, ~3,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 4.0 m
Radar Cross Section
9.231 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 YAOGAN 26
1 40362U 14088A 26172.53086809 .00017149 00000-0 33512-3 0 9992
2 40362 97.0643 172.6381 0005541 57.7340 302.4447 15.47500088638374Epoch: 2026-06-21T12:44Z
TLE epoch observation values (Epoch: 2026-06-21T12:44:27.002Z)
Latitude
-0.00008°
Longitude
71.79579°
Altitude
425.158 km
Speed
7.657 km/s
True Right ascension
11h 30m 33s
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
00:51:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
424.724 km
Perigee altitude
417.189 km
Semi-major axis
6,799.094 km
Eccentricity
0.00055
Inclination
97.0643°
RAAN
172.6381°
Arg. of periapsis
57.734°
True anomaly
302.3911°
Mean anomaly
302.4447°
Eccentric anomaly
302.4179°
Mean motion
3.87139 °/min
Orbital period
92.99 mins
BSTAR
0.00033512
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Other satellites on launch #88 in the year 2014 (2014-12-27 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.YAOGAN 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-23 00:34:45.150Z | 215.487° SW | 2026-06-23 00:35:45.150Z | 244.39° WSW | 26.884° | 2026-06-23 00:38:45.150Z | 325.017° NNW |
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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