YAOGAN-43 02E, 60949
Orbit data source: Space-Track
YAOGAN-43 02E, 60949 is a payload satellite owned by PLA GAD (CN) in LEO that was launched on Tue, 03 Sep 2024 UTC via a CHANG ZHENG 4B 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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60949 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Operational Defense Communications
Bus & Motor
Unknown
Mass
~300 kg wet, ~300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
11.063 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 YAOGAN-43 02E
1 60949U 24156E 26256.74869468 .00010601 00000-0 44046-3 0 9998
2 60949 34.9984 1.1975 0005222 39.5643 320.5452 15.23028513112950Epoch: 2026-09-13T17:58Z
TLE epoch observation values (Epoch: 2026-09-13T17:58:07.220Z)
Latitude
-0.00002°
Longitude
98.9285°
Altitude
492.848 km
Speed
7.622 km/s
True Right ascension
00h 04m 47s
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
16:55:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.554 km
Perigee altitude
496.371 km
Semi-major axis
6,878.099 km
Eccentricity
0.00052
Inclination
34.9984°
RAAN
1.1975°
Arg. of periapsis
39.5643°
True anomaly
320.50715°
Mean anomaly
320.5452°
Eccentric anomaly
320.52618°
Mean motion
3.80488 °/min
Orbital period
94.62 mins
BSTAR
0.00044046
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Other satellites on launch #156 in the year 2024 (2024-09-03 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-43 02E 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 | 2026-09-14 11:32:24.971Z | 219.776° SW | 2026-09-14 11:35:24.971Z | 156.856° SSE | 27.389° | 2026-09-14 11:38:24.971Z | 105.946° ESE |
| 5 mins | 2026-09-14 13:12:24.971Z | 239.035° WSW | 2026-09-14 13:14:24.971Z | 187.216° SSW | 39.345° | 2026-09-14 13:17:24.971Z | 115.491° SE |
| 4 mins | 2026-09-14 14:52:24.971Z | 233.573° WSW | 2026-09-14 14:54:24.971Z | 184.237° SSW | 25.837° | 2026-09-14 14:56:24.971Z | 145.82° 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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