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 57945U 26145.66668980 +.00000000 +00000-0 +10915-2 0 00008
2 57945 53.1597 26.5782 0001223 94.1884 138.9971 15.34376589 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001223 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 26.5782° |
| argument of perigee: | 94.1884° |
| revolutions per day: | 15.34376589 |
| mean anomaly at epoch: | 138.9971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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