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 57946U 26145.60317365 +.00000000 +00000-0 +92774-4 0 00006
2 57946 53.1603 104.1875 0001869 82.2231 277.8981 15.30180376 05
| Epoch (UTC): | 25 May 2026 14:28:34 |
| Eccentricity: | 0.0001869 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 104.1875° |
| argument of perigee: | 82.2231° |
| revolutions per day: | 15.30180376 |
| mean anomaly at epoch: | 277.8981° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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