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 58935U 26145.49694083 +.00000000 +00000-0 +74424-4 0 00009
2 58935 53.1597 313.1611 0001070 93.9549 266.1574 15.30200906 02
| Epoch (UTC): | 25 May 2026 11:55:35 |
| Eccentricity: | 0.0001070 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.1611° |
| argument of perigee: | 93.9549° |
| revolutions per day: | 15.30200906 |
| mean anomaly at epoch: | 266.1574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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