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 26066.17577718 +.00000000 +00000-0 +35987-3 0 00007
2 60235 61.9930 225.9420 0060687 112.1209 248.6339 15.00619953 07
| Epoch (UTC): | 07 March 2026 04:13:07 |
| Eccentricity: | 0.0060687 |
| inclination: | 61.9930° |
| perigee height: | 523 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 225.9420° |
| argument of perigee: | 112.1209° |
| revolutions per day: | 15.00619953 |
| mean anomaly at epoch: | 248.6339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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