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 53799U 26144.65574979 +.00000000 +00000-0 +61728-4 0 00003
2 53799 53.2150 283.1665 0001505 89.1482 270.9683 15.08843730 09
| Epoch (UTC): | 24 May 2026 15:44:16 |
| Eccentricity: | 0.0001505 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 283.1665° |
| argument of perigee: | 89.1482° |
| revolutions per day: | 15.08843730 |
| mean anomaly at epoch: | 270.9683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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