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 65778U 26145.43903309 +.00000000 +00000-0 +48479-3 0 00000
2 65778 51.9024 56.2153 0000949 91.9699 268.1372 14.79936042 07
| Epoch (UTC): | 25 May 2026 10:32:12 |
| Eccentricity: | 0.0000949 |
| inclination: | 51.9024° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 56.2153° |
| argument of perigee: | 91.9699° |
| revolutions per day: | 14.79936042 |
| mean anomaly at epoch: | 268.1372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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