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 58093U 26145.29812613 +.00000000 +00000-0 -91595-5 0 00003
2 58093 43.0037 5.0966 0000761 273.0016 87.0748 15.27583248 02
| Epoch (UTC): | 25 May 2026 07:09:18 |
| Eccentricity: | 0.0000761 |
| inclination: | 43.0037° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.0966° |
| argument of perigee: | 273.0016° |
| revolutions per day: | 15.27583248 |
| mean anomaly at epoch: | 87.0748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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