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 26066.30904596 +.00000000 +00000-0 +36939-3 0 00008
2 60235 61.9930 225.4788 0060671 112.1503 248.6041 15.00621611 03
| Epoch (UTC): | 07 March 2026 07:25:01 |
| Eccentricity: | 0.0060671 |
| inclination: | 61.9930° |
| perigee height: | 523 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 225.4788° |
| argument of perigee: | 112.1503° |
| revolutions per day: | 15.00621611 |
| mean anomaly at epoch: | 248.6041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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