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 58602U 26145.47469293 +.00000000 +00000-0 +94025-4 0 00000
2 58602 43.0027 295.0373 0001764 280.1974 79.8678 15.27579789 02
| Epoch (UTC): | 25 May 2026 11:23:33 |
| Eccentricity: | 0.0001764 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.0373° |
| argument of perigee: | 280.1974° |
| revolutions per day: | 15.27579789 |
| mean anomaly at epoch: | 79.8678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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