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 57859U 26145.38515127 +.00000000 +00000-0 +26321-4 0 00005
2 57859 53.1612 287.6507 0001217 91.4514 268.6626 15.30193327 04
| Epoch (UTC): | 25 May 2026 09:14:37 |
| Eccentricity: | 0.0001217 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.6507° |
| argument of perigee: | 91.4514° |
| revolutions per day: | 15.30193327 |
| mean anomaly at epoch: | 268.6626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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