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 59767U 26145.40684546 +.00000000 +00000-0 +18575-3 0 00001
2 59767 53.1590 30.2966 0001283 97.2525 262.8622 15.31676552 08
| Epoch (UTC): | 25 May 2026 09:45:51 |
| Eccentricity: | 0.0001283 |
| inclination: | 53.1590° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 30.2966° |
| argument of perigee: | 97.2525° |
| revolutions per day: | 15.31676552 |
| mean anomaly at epoch: | 262.8622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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