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 53545U 26145.53797824 +.00000000 +00000-0 +23580-3 0 00009
2 53545 53.2152 79.1305 0001510 67.8804 292.2348 15.08853919 06
| Epoch (UTC): | 25 May 2026 12:54:41 |
| Eccentricity: | 0.0001510 |
| inclination: | 53.2152° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 79.1305° |
| argument of perigee: | 67.8804° |
| revolutions per day: | 15.08853919 |
| mean anomaly at epoch: | 292.2348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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