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 26162.00731442 +.00000000 +00000-0 +17614-3 0 00006
2 53807 53.2295 62.9824 0006787 143.3962 216.7508 15.38193785 07
| Epoch (UTC): | 11 June 2026 00:10:31 |
| Eccentricity: | 0.0006787 |
| inclination: | 53.2295° |
| perigee height: | 447 km |
| apogee height: | 456 km |
| right ascension of ascending node: | 62.9824° |
| argument of perigee: | 143.3962° |
| revolutions per day: | 15.38193785 |
| mean anomaly at epoch: | 216.7508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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