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 53563U 26145.20773068 +.00000000 +00000-0 -13929-3 0 00004
2 53563 53.2123 70.8421 0001582 76.2965 283.8203 15.08850055 06
| Epoch (UTC): | 25 May 2026 04:59:07 |
| Eccentricity: | 0.0001582 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 70.8421° |
| argument of perigee: | 76.2965° |
| revolutions per day: | 15.08850055 |
| mean anomaly at epoch: | 283.8203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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