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 51780U 26145.61388727 +.00000000 +00000-0 -16892-3 0 00004
2 51780 53.2110 353.7835 0001693 96.1948 263.9237 15.08846904 02
| Epoch (UTC): | 25 May 2026 14:43:59 |
| Eccentricity: | 0.0001693 |
| inclination: | 53.2110° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 353.7835° |
| argument of perigee: | 96.1948° |
| revolutions per day: | 15.08846904 |
| mean anomaly at epoch: | 263.9237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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