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 58211U 26145.40159449 +.00000000 +00000-0 -17108-3 0 00005
2 58211 43.0029 120.8148 0001342 259.3758 100.6943 15.27540989 03
| Epoch (UTC): | 25 May 2026 09:38:17 |
| Eccentricity: | 0.0001342 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 120.8148° |
| argument of perigee: | 259.3758° |
| revolutions per day: | 15.27540989 |
| mean anomaly at epoch: | 100.6943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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