YAOGAN-43 02D, 60948
Orbit data source: Space-Track
YAOGAN-43 02D, 60948 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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60948 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: 9 hours ago
TLE from 9 hours ago
0 YAOGAN-43 02D
1 60948U 24156D 26256.61343042 .00001004 00000-0 43241-4 0 9992
2 60948 34.9944 1.7933 0003780 313.9324 46.1078 15.22970739112935Epoch: 2026-09-13T14:43Z
TLE epoch observation values (Epoch: 2026-09-13T14:43:20.388Z)
Latitude
-0.00003°
Longitude
148.35274°
Altitude
493.991 km
Speed
7.621 km/s
True Right ascension
00h 07m 10s
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
16:02:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
502.737 km
Perigee altitude
497.537 km
Semi-major axis
6,878.274 km
Eccentricity
0.00038
Inclination
34.9944°
RAAN
1.7933°
Arg. of periapsis
313.9324°
True anomaly
46.13903°
Mean anomaly
46.1078°
Eccentric anomaly
46.12341°
Mean motion
3.80473 °/min
Orbital period
94.62 mins
BSTAR
0.000043241
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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 02D 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 | 2026-09-14 11:26:24.619Z | 216.106° SW | 2026-09-14 11:29:24.619Z | 151.425° SSE | 26.133° | 2026-09-14 11:31:24.619Z | 113.805° SE |
| 5 mins | 2026-09-14 13:06:24.619Z | 235.945° WSW | 2026-09-14 13:08:24.619Z | 178.666° S | 39.783° | 2026-09-14 13:11:24.619Z | 113.428° SE |
| 4 mins | 2026-09-14 14:46:24.619Z | 230.82° WSW | 2026-09-14 14:47:24.619Z | 207.178° SW | 26.922° | 2026-09-14 14:50:24.619Z | 142.361° 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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