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 57978U 26145.39494463 +.00000000 +00000-0 +53227-4 0 00002
2 57978 43.0021 277.5650 0001406 264.1328 95.9364 15.27575818 02
| Epoch (UTC): | 25 May 2026 09:28:43 |
| Eccentricity: | 0.0001406 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.5650° |
| argument of perigee: | 264.1328° |
| revolutions per day: | 15.27575818 |
| mean anomaly at epoch: | 95.9364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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