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 58995U 26145.60615279 +.00000000 +00000-0 +00000-0 0 00003
2 58995 0.0184 288.0114 0001551 130.3590 155.9953 1.00271220 00
| Epoch (UTC): | 25 May 2026 14:32:51 |
| Eccentricity: | 0.0001551 |
| inclination: | 0.0184° |
| perigee height: | 35780 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 288.0114° |
| argument of perigee: | 130.3590° |
| revolutions per day: | 1.00271220 |
| mean anomaly at epoch: | 155.9953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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