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 60235U 26066.64221780 +.00000000 +00000-0 +41053-3 0 00005
2 60235 61.9931 224.3208 0060633 112.2157 248.5381 15.00625859 07
| Epoch (UTC): | 07 March 2026 15:24:47 |
| Eccentricity: | 0.0060633 |
| inclination: | 61.9931° |
| perigee height: | 523 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 224.3208° |
| argument of perigee: | 112.2157° |
| revolutions per day: | 15.00625859 |
| mean anomaly at epoch: | 248.5381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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