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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Edit Public Description
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: 8 hours ago
TLE from 8 hours ago
0 YAOGAN-43 02D
1 60948U 24156D 25341.97060118 .00014319 00000-0 59453-3 0 9999
2 60948 34.9935 320.5888 0005030 322.8805 37.1561 15.23004736 70272Epoch: 2025-12-07T23:17Z
TLE epoch observation values (Epoch: 2025-12-07T23:17:39.941Z)
Latitude
-0.00005°
Longitude
-105.80404°
Altitude
492.935 km
Speed
7.622 km/s
True Right ascension
21h 22m 21s
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
05:47:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.494 km
Perigee altitude
496.575 km
Semi-major axis
6,878.172 km
Eccentricity
0.0005
Inclination
34.9935°
RAAN
320.5888°
Arg. of periapsis
322.8805°
True anomaly
37.19093°
Mean anomaly
37.1561°
Eccentric anomaly
37.17351°
Mean motion
3.80482 °/min
Orbital period
94.62 mins
BSTAR
0.00059453
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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 | 2025-12-08 07:38:22.706Z | 243.525° WSW | 2025-12-08 07:41:22.706Z | 192.971° SSW | 15.854° | 2025-12-08 07:43:22.706Z | 161.91° S |
| 4 mins | 2025-12-09 02:17:22.706Z | 188.274° SSW | 2025-12-09 02:18:22.706Z | 169.457° S | 17.624° | 2025-12-09 02:21:22.706Z | 115.673° SE |
| 5 mins | 2025-12-09 03:56:22.706Z | 225.123° WSW | 2025-12-09 03:58:22.706Z | 167.238° S | 30.572° | 2025-12-09 04:01:22.706Z | 108.529° ESE |
| 5 mins | 2025-12-09 05:35:22.706Z | 244.685° WSW | 2025-12-09 05:37:22.706Z | 200.385° SSW | 28.871° | 2025-12-09 05:40:22.706Z | 129.508° 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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