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 59432U 26145.39725427 +.00000000 +00000-0 +26728-4 0 00002
2 59432 53.1607 285.3693 0001347 115.7685 244.3455 15.30191814 01
| Epoch (UTC): | 25 May 2026 09:32:02 |
| Eccentricity: | 0.0001347 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 285.3693° |
| argument of perigee: | 115.7685° |
| revolutions per day: | 15.30191814 |
| mean anomaly at epoch: | 244.3455° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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