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 57060U 26145.42748209 +.00000000 +00000-0 +51950-5 0 00000
2 57060 43.0080 37.6892 0001699 266.4933 93.5724 15.27579780 09
| Epoch (UTC): | 25 May 2026 10:15:34 |
| Eccentricity: | 0.0001699 |
| inclination: | 43.0080° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 37.6892° |
| argument of perigee: | 266.4933° |
| revolutions per day: | 15.27579780 |
| mean anomaly at epoch: | 93.5724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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