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 53807U 26105.33642053 +.00000000 +00000-0 +44095-4 0 00002
2 53807 53.2306 328.8665 0005785 2.9294 357.1744 15.37578837 08
| Epoch (UTC): | 15 April 2026 08:04:26 |
| Eccentricity: | 0.0005785 |
| inclination: | 53.2306° |
| perigee height: | 449 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 328.8665° |
| argument of perigee: | 2.9294° |
| revolutions per day: | 15.37578837 |
| mean anomaly at epoch: | 357.1744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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