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 43762U 26145.55330069 +.00000000 +00000-0 +27292-3 0 00009
2 43762 97.4103 195.9561 0004573 69.1776 290.9945 15.13463131 05
| Epoch (UTC): | 25 May 2026 13:16:45 |
| Eccentricity: | 0.0004573 |
| inclination: | 97.4103° |
| perigee height: | 522 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 195.9561° |
| argument of perigee: | 69.1776° |
| revolutions per day: | 15.13463131 |
| mean anomaly at epoch: | 290.9945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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