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 59437U 26145.37351193 +.00000000 +00000-0 +43203-4 0 00007
2 59437 53.1606 287.3675 0000971 104.4332 255.6777 15.30193920 05
| Epoch (UTC): | 25 May 2026 08:57:51 |
| Eccentricity: | 0.0000971 |
| inclination: | 53.1606° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.3675° |
| argument of perigee: | 104.4332° |
| revolutions per day: | 15.30193920 |
| mean anomaly at epoch: | 255.6777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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