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 53547U 26145.53063507 +.00000000 +00000-0 +52822-4 0 00007
2 53547 53.2129 79.1656 0001432 85.8692 274.2464 15.08839341 01
| Epoch (UTC): | 25 May 2026 12:44:06 |
| Eccentricity: | 0.0001432 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 79.1656° |
| argument of perigee: | 85.8692° |
| revolutions per day: | 15.08839341 |
| mean anomaly at epoch: | 274.2464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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