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 53561U 26145.08902490 +.00000000 +00000-0 +59952-4 0 00007
2 53561 53.2152 81.1481 0001368 86.6509 273.4640 15.08841501 04
| Epoch (UTC): | 25 May 2026 02:08:11 |
| Eccentricity: | 0.0001368 |
| inclination: | 53.2152° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 81.1481° |
| argument of perigee: | 86.6509° |
| revolutions per day: | 15.08841501 |
| mean anomaly at epoch: | 273.4640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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