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 60523U 26145.22709722 +.00000000 +00000-0 +69518-3 0 00000
2 60523 97.3780 243.8972 0002875 249.8734 110.2231 15.91905521 04
| Epoch (UTC): | 25 May 2026 05:27:01 |
| Eccentricity: | 0.0002875 |
| inclination: | 97.3780° |
| perigee height: | 295 km |
| apogee height: | 299 km |
| right ascension of ascending node: | 243.8972° |
| argument of perigee: | 249.8734° |
| revolutions per day: | 15.91905521 |
| mean anomaly at epoch: | 110.2231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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