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 57968U 26145.37108866 +.00000000 +00000-0 +42609-4 0 00000
2 57968 43.0013 262.9666 0000958 282.2922 77.7823 15.27574280 09
| Epoch (UTC): | 25 May 2026 08:54:22 |
| Eccentricity: | 0.0000958 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 262.9666° |
| argument of perigee: | 282.2922° |
| revolutions per day: | 15.27574280 |
| mean anomaly at epoch: | 77.7823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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