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 59755U 26145.49569461 +.00000000 +00000-0 +85124-5 0 00001
2 59755 53.1593 187.8545 0001068 90.5286 269.5854 15.69705637 00
| Epoch (UTC): | 25 May 2026 11:53:48 |
| Eccentricity: | 0.0001068 |
| inclination: | 53.1593° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 187.8545° |
| argument of perigee: | 90.5286° |
| revolutions per day: | 15.69705637 |
| mean anomaly at epoch: | 269.5854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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