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 53017U 26145.66668980 +.00000000 +00000-0 +17117-1 0 00004
2 53017 53.2139 92.7860 0001686 90.3665 71.9869 15.38973014 04
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001686 |
| inclination: | 53.2139° |
| perigee height: | 448 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 92.7860° |
| argument of perigee: | 90.3665° |
| revolutions per day: | 15.38973014 |
| mean anomaly at epoch: | 71.9869° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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