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 51747U 26145.26709240 +.00000000 +00000-0 -14665-4 0 00002
2 51747 53.2165 335.3986 0001258 88.0135 272.1002 15.08835183 02
| Epoch (UTC): | 25 May 2026 06:24:36 |
| Eccentricity: | 0.0001258 |
| inclination: | 53.2165° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 335.3986° |
| argument of perigee: | 88.0135° |
| revolutions per day: | 15.08835183 |
| mean anomaly at epoch: | 272.1002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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