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 59779U 26145.58378295 +.00000000 +00000-0 +69878-4 0 00007
2 59779 98.6673 264.6516 0010701 274.8477 85.1484 14.31836170 00
| Epoch (UTC): | 25 May 2026 14:00:38 |
| Eccentricity: | 0.0010701 |
| inclination: | 98.6673° |
| perigee height: | 778 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 264.6516° |
| argument of perigee: | 274.8477° |
| revolutions per day: | 14.31836170 |
| mean anomaly at epoch: | 85.1484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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