YAOGAN-30 N, 44449
Orbit data source: Space-Track
YAOGAN-30 N, 44449 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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44449 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 N
1 44449U 19045A 26172.49240306 .00001965 00000-0 14632-3 0 9990
2 44449 34.9946 303.8549 0004513 309.7066 50.3245 15.02713722377262Epoch: 2026-06-21T11:49Z
TLE epoch observation values (Epoch: 2026-06-21T11:49:03.624Z)
Latitude
0.00004°
Longitude
-143.10204°
Altitude
555.451 km
Speed
7.587 km/s
True Right ascension
20h 15m 25s
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
21:23:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
564.887 km
Perigee altitude
558.623 km
Semi-major axis
6,939.892 km
Eccentricity
0.00045
Inclination
34.9946°
RAAN
303.8549°
Arg. of periapsis
309.7066°
True anomaly
50.36432°
Mean anomaly
50.3245°
Eccentric anomaly
50.34441°
Mean motion
3.75417 °/min
Orbital period
95.89 mins
BSTAR
0.00014632
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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 N 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 | 2026-06-22 11:57:33.170Z | 189.007° SSW | 2026-06-22 11:59:33.170Z | 157.505° S | 16.151° | 2026-06-22 12:01:33.170Z | 124.954° SE |
| 6 mins | 2026-06-22 13:37:33.170Z | 229.268° WSW | 2026-06-22 13:40:33.170Z | 162.766° S | 30.367° | 2026-06-22 13:43:33.170Z | 107.382° ESE |
| 6 mins | 2026-06-22 15:18:33.170Z | 247.065° WSW | 2026-06-22 15:21:33.170Z | 173.442° S | 32.495° | 2026-06-22 15:24:33.170Z | 119.344° SE |
| 4 mins | 2026-06-22 17:00:33.170Z | 229.524° WSW | 2026-06-22 17:01:33.170Z | 210.436° SW | 20.435° | 2026-06-22 17:04:33.170Z | 156.466° 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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