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 60047U 26145.28502825 +.00000000 +00000-0 +25267-4 0 00006
2 60047 53.1598 248.4979 0000757 81.9186 278.1917 15.69719825 03
| Epoch (UTC): | 25 May 2026 06:50:26 |
| Eccentricity: | 0.0000757 |
| inclination: | 53.1598° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 248.4979° |
| argument of perigee: | 81.9186° |
| revolutions per day: | 15.69719825 |
| mean anomaly at epoch: | 278.1917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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