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 53575U 26145.49841256 +.00000000 +00000-0 +28045-3 0 00007
2 53575 53.2138 69.1029 0001366 94.7331 265.3817 15.08813530 05
| Epoch (UTC): | 25 May 2026 11:57:42 |
| Eccentricity: | 0.0001366 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 69.1029° |
| argument of perigee: | 94.7331° |
| revolutions per day: | 15.08813530 |
| mean anomaly at epoch: | 265.3817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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