YAOGAN-30 R, 45460
Orbit data source: Space-Track
YAOGAN-30 R, 45460 is a payload satellite owned by PLA SSF (CN) in LEO that was launched on Tue, 24 Mar 2020 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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45460 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: 23 hours ago
TLE from 23 hours ago
0 YAOGAN-30 R
1 45460U 20021A 26172.48360558 .00001392 00000-0 10427-3 0 9993
2 45460 34.9934 184.6887 0002916 50.6489 309.4477 15.02730765341205Epoch: 2026-06-21T11:36Z
TLE epoch observation values (Epoch: 2026-06-21T11:36:23.522Z)
Latitude
-0.00002°
Longitude
100.90744°
Altitude
556.112 km
Speed
7.587 km/s
True Right ascension
12h 18m 45s
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
21:33:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.726 km
Perigee altitude
559.679 km
Semi-major axis
6,939.839 km
Eccentricity
0.00029
Inclination
34.9934°
RAAN
184.6887°
Arg. of periapsis
50.6489°
True anomaly
309.42189°
Mean anomaly
309.4477°
Eccentric anomaly
309.4348°
Mean motion
3.75421 °/min
Orbital period
95.89 mins
BSTAR
0.00010427
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Other satellites on launch #21 in the year 2020 (2020-03-24 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 R 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 03:41:24.604Z | 190.497° SSW | 2026-06-23 03:43:24.604Z | 159.795° S | 15.932° | 2026-06-23 03:45:24.604Z | 126.757° SE |
| 5 mins | 2026-06-23 05:22:24.604Z | 218.979° SW | 2026-06-23 05:24:24.604Z | 166.994° S | 30.328° | 2026-06-23 05:27:24.604Z | 108.285° ESE |
| 6 mins | 2026-06-23 07:02:24.604Z | 248.059° W | 2026-06-23 07:05:24.604Z | 177.854° S | 32.646° | 2026-06-23 07:08:24.604Z | 119.963° SE |
| 4 mins | 2026-06-23 08:44:24.604Z | 231.409° WSW | 2026-06-23 08:46:24.604Z | 191.189° SSW | 20.441° | 2026-06-23 08:48:24.604Z | 157.543° S |
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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