YAOGAN-30 AD, 49026
Orbit data source: Space-Track
YAOGAN-30 AD, 49026 is a payload satellite owned by PLA SSF (CN) in LEO that was launched on Mon, 19 Jul 2021 UTC via a CHANG ZHENG 2C launch vehicle from the Xichang Space Center, China (XSC). 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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49026 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Operational Defense Sigint
Bus & Motor
Unknown
Mass
~500 kg wet, ~500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.446 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 YAOGAN-30 AD
1 49026U 21065A 26172.50765637 .00001816 00000-0 13534-3 0 9997
2 49026 34.9932 246.7776 0004491 199.9011 160.1523 15.02729129269294Epoch: 2026-06-21T12:11Z
TLE epoch observation values (Epoch: 2026-06-21T12:11:01.510Z)
Latitude
0.00002°
Longitude
154.31441°
Altitude
560.331 km
Speed
7.582 km/s
True Right ascension
16h 27m 06s
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
23:07:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
564.824 km
Perigee altitude
558.591 km
Semi-major axis
6,939.845 km
Eccentricity
0.00045
Inclination
34.9932°
RAAN
246.7776°
Arg. of periapsis
199.9011°
True anomaly
160.16976°
Mean anomaly
160.1523°
Eccentric anomaly
160.16103°
Mean motion
3.75421 °/min
Orbital period
95.89 mins
BSTAR
0.00013534
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Other satellites on launch #65 in the year 2021 (2021-07-19 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-30 AD 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 12:32:02.037Z | 248.719° W | 2026-06-22 12:35:02.037Z | 187.033° SSW | 27.001° | 2026-06-22 12:38:02.037Z | 135.28° SSE |
| 6 mins | 2026-06-23 09:07:02.037Z | 218.243° SW | 2026-06-23 09:09:02.037Z | 176.601° S | 28.022° | 2026-06-23 09:13:02.037Z | 103.868° ESE |
| 6 mins | 2026-06-23 10:48:02.037Z | 240.228° WSW | 2026-06-23 10:50:02.037Z | 190.48° SSW | 33.534° | 2026-06-23 10:54:02.037Z | 112.603° SE |
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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