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 53758U 26145.49347402 +.00000000 +00000-0 +59549-4 0 00008
2 53758 53.5285 146.7219 0007776 273.1902 86.8184 14.61899596 02
| Epoch (UTC): | 25 May 2026 11:50:36 |
| Eccentricity: | 0.0007776 |
| inclination: | 53.5285° |
| perigee height: | 682 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 146.7219° |
| argument of perigee: | 273.1902° |
| revolutions per day: | 14.61899596 |
| mean anomaly at epoch: | 86.8184° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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