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 53830U 26144.86454550 +.00000000 +00000-0 +12684-3 0 00000
2 53830 53.2129 321.9862 0001674 79.3881 280.7299 15.08825516 06
| Epoch (UTC): | 24 May 2026 20:44:56 |
| Eccentricity: | 0.0001674 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 321.9862° |
| argument of perigee: | 79.3881° |
| revolutions per day: | 15.08825516 |
| mean anomaly at epoch: | 280.7299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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