YAOGAN-43 02A, 60945
Orbit data source: Space-Track
YAOGAN-43 02A, 60945 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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60945 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: 5 hours ago
TLE from 5 hours ago
0 YAOGAN-43 02A
1 60945U 24156A 26256.79619830 .00059476 00000-0 75375-3 0 9997
2 60945 34.9939 288.8209 0001949 180.1226 179.9499 15.58311726113757Epoch: 2026-09-13T19:06Z
TLE epoch observation values (Epoch: 2026-09-13T19:06:31.533Z)
Latitude
-0.00002°
Longitude
9.40377°
Altitude
392.752 km
Speed
7.676 km/s
True Right ascension
19h 15m 17s
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
16:55:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
397.164 km
Perigee altitude
394.524 km
Semi-major axis
6,773.981 km
Eccentricity
0.00019
Inclination
34.9939°
RAAN
288.8209°
Arg. of periapsis
180.1226°
True anomaly
179.94992°
Mean anomaly
179.9499°
Eccentric anomaly
179.94991°
Mean motion
3.89294 °/min
Orbital period
92.48 mins
BSTAR
0.00075375
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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 02A 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 | 2026-09-14 07:43:58.717Z | 219.767° SW | 2026-09-14 07:44:58.717Z | 192.042° SSW | 29.2° | 2026-09-14 07:47:58.717Z | 112.654° SE |
| 4 mins | 2026-09-14 09:20:58.717Z | 235.213° WSW | 2026-09-14 09:22:58.717Z | 172.908° S | 27.992° | 2026-09-14 09:24:58.717Z | 130.159° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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