YAOGAN-30 P, 44450
Orbit data source: Space-Track
YAOGAN-30 P, 44450 is a payload satellite owned by PLA SSF (CN) in LEO that was launched on Fri, 26 Jul 2019 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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44450 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: 22 hours ago
TLE from 22 hours ago
0 YAOGAN-30 P
1 44450U 19045B 26172.53638376 .00002043 00000-0 15202-3 0 9997
2 44450 34.9931 303.1176 0007741 113.5921 246.5600 15.02713377377310Epoch: 2026-06-21T12:52Z
TLE epoch observation values (Epoch: 2026-06-21T12:52:23.556Z)
Latitude
-0.00007°
Longitude
-159.71589°
Altitude
559.589 km
Speed
7.583 km/s
True Right ascension
20h 12m 28s
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
21:29:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
567.128 km
Perigee altitude
556.384 km
Semi-major axis
6,939.893 km
Eccentricity
0.00077
Inclination
34.9931°
RAAN
303.1176°
Arg. of periapsis
113.5921°
True anomaly
246.47865°
Mean anomaly
246.56°
Eccentric anomaly
246.51932°
Mean motion
3.75417 °/min
Orbital period
95.89 mins
BSTAR
0.00015202
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Other satellites on launch #45 in the year 2019 (2019-07-26 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 P 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-22 13:04:11.533Z | 212.471° SW | 2026-06-22 13:06:11.533Z | 170.199° S | 26.402° | 2026-06-22 13:09:11.533Z | 110.674° ESE |
| 5 mins | 2026-06-22 14:45:11.533Z | 236.66° WSW | 2026-06-22 14:47:11.533Z | 181.843° SSW | 33.733° | 2026-06-22 14:50:11.533Z | 115.318° SE |
| 5 mins | 2026-06-22 16:26:11.533Z | 237.395° WSW | 2026-06-22 16:28:11.533Z | 192.355° SSW | 25.333° | 2026-06-22 16:31:11.533Z | 139.829° 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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