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 51868U 26144.94504529 +.00000000 +00000-0 +64599-4 0 00003
2 51868 53.2150 26.7987 0001448 86.0105 274.1052 15.08839810 06
| Epoch (UTC): | 24 May 2026 22:40:51 |
| Eccentricity: | 0.0001448 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 26.7987° |
| argument of perigee: | 86.0105° |
| revolutions per day: | 15.08839810 |
| mean anomaly at epoch: | 274.1052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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