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 58718U 26145.61933765 +.00000000 +00000-0 -68128-5 0 00001
2 58718 53.1600 232.5990 0000961 104.8548 255.2559 15.30184793 06
| Epoch (UTC): | 25 May 2026 14:51:50 |
| Eccentricity: | 0.0000961 |
| inclination: | 53.1600° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.5990° |
| argument of perigee: | 104.8548° |
| revolutions per day: | 15.30184793 |
| mean anomaly at epoch: | 255.2559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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