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 57495U 26145.62634344 +.00000000 +00000-0 +36507-4 0 00008
2 57495 43.0029 301.3932 0001650 259.6507 100.4159 15.27579624 05
| Epoch (UTC): | 25 May 2026 15:01:56 |
| Eccentricity: | 0.0001650 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 301.3932° |
| argument of perigee: | 259.6507° |
| revolutions per day: | 15.27579624 |
| mean anomaly at epoch: | 100.4159° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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