View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 58212U 26145.38242872 +.00000000 +00000-0 +28508-4 0 00002
2 58212 43.0027 121.5117 0001118 299.3702 60.7038 15.27579632 08
| Epoch (UTC): | 25 May 2026 09:10:41 |
| Eccentricity: | 0.0001118 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 121.5117° |
| argument of perigee: | 299.3702° |
| revolutions per day: | 15.27579632 |
| mean anomaly at epoch: | 60.7038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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