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 53626U 26145.55174213 +.00000000 +00000-0 +13860-4 0 00003
2 53626 53.2133 248.7125 0001118 97.5654 262.5465 15.08841813 06
| Epoch (UTC): | 25 May 2026 13:14:30 |
| Eccentricity: | 0.0001118 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 248.7125° |
| argument of perigee: | 97.5654° |
| revolutions per day: | 15.08841813 |
| mean anomaly at epoch: | 262.5465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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