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 60906U 26145.61936274 +.00000000 +00000-0 +10626-4 0 00009
2 60906 53.1598 112.2814 0001188 95.9467 264.1686 15.69707748 08
| Epoch (UTC): | 25 May 2026 14:51:52 |
| Eccentricity: | 0.0001188 |
| inclination: | 53.1598° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 112.2814° |
| argument of perigee: | 95.9467° |
| revolutions per day: | 15.69707748 |
| mean anomaly at epoch: | 264.1686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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