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 58065U 26145.47630127 +.00000000 +00000-0 +19508-3 0 00001
2 58065 43.0030 313.3890 0001588 255.0383 105.0293 15.27556175 05
| Epoch (UTC): | 25 May 2026 11:25:52 |
| Eccentricity: | 0.0001588 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.3890° |
| argument of perigee: | 255.0383° |
| revolutions per day: | 15.27556175 |
| mean anomaly at epoch: | 105.0293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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