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 53826U 26145.47174589 +.00000000 +00000-0 +10183-3 0 00006
2 53826 53.2130 319.3772 0001255 91.2913 268.8223 15.08828132 09
| Epoch (UTC): | 25 May 2026 11:19:18 |
| Eccentricity: | 0.0001255 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 319.3772° |
| argument of perigee: | 91.2913° |
| revolutions per day: | 15.08828132 |
| mean anomaly at epoch: | 268.8223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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