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 58159U 26145.58935429 +.00000000 +00000-0 +12044-4 0 00009
2 58159 53.1605 222.3748 0000979 106.7798 253.3311 15.31694954 06
| Epoch (UTC): | 25 May 2026 14:08:40 |
| Eccentricity: | 0.0000979 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 222.3748° |
| argument of perigee: | 106.7798° |
| revolutions per day: | 15.31694954 |
| mean anomaly at epoch: | 253.3311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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