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 58973U 26145.43733352 +.00000000 +00000-0 +16944-4 0 00001
2 58973 53.1611 300.2036 0001197 79.6131 280.5005 15.30194126 02
| Epoch (UTC): | 25 May 2026 10:29:45 |
| Eccentricity: | 0.0001197 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.2036° |
| argument of perigee: | 79.6131° |
| revolutions per day: | 15.30194126 |
| mean anomaly at epoch: | 280.5005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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