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 59264U 26145.54392377 +.00000000 +00000-0 +63483-3 0 00004
2 59264 53.1569 184.1306 0000631 91.9854 268.1219 15.30231687 01
| Epoch (UTC): | 25 May 2026 13:03:15 |
| Eccentricity: | 0.0000631 |
| inclination: | 53.1569° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.1306° |
| argument of perigee: | 91.9854° |
| revolutions per day: | 15.30231687 |
| mean anomaly at epoch: | 268.1219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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