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 59446U 26145.07625846 +.00000000 +00000-0 +11482-3 0 00006
2 59446 45.6114 36.6818 0003500 275.6163 84.4319 14.99055020 05
| Epoch (UTC): | 25 May 2026 01:49:48 |
| Eccentricity: | 0.0003500 |
| inclination: | 45.6114° |
| perigee height: | 567 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 36.6818° |
| argument of perigee: | 275.6163° |
| revolutions per day: | 14.99055020 |
| mean anomaly at epoch: | 84.4319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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