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 51957U 26145.40415936 +.00000000 +00000-0 +84582-5 0 00002
2 51957 53.1626 40.0674 0001374 86.5345 273.5813 15.31702670 00
| Epoch (UTC): | 25 May 2026 09:41:59 |
| Eccentricity: | 0.0001374 |
| inclination: | 53.1626° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 40.0674° |
| argument of perigee: | 86.5345° |
| revolutions per day: | 15.31702670 |
| mean anomaly at epoch: | 273.5813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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