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 59955U 26145.63399215 +.00000000 +00000-0 -88788-5 0 00007
2 59955 53.1587 231.7613 0001285 81.1390 278.9774 15.69716048 06
| Epoch (UTC): | 25 May 2026 15:12:56 |
| Eccentricity: | 0.0001285 |
| inclination: | 53.1587° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 231.7613° |
| argument of perigee: | 81.1390° |
| revolutions per day: | 15.69716048 |
| mean anomaly at epoch: | 278.9774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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