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 26019.32641372 +.00000000 +00000-0 +23485-3 0 00000
2 60235 61.9946 28.7302 0063294 101.3660 259.4550 15.00262158 06
| Epoch (UTC): | 19 January 2026 07:50:02 |
| Eccentricity: | 0.0063294 |
| inclination: | 61.9946° |
| perigee height: | 522 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 28.7302° |
| argument of perigee: | 101.3660° |
| revolutions per day: | 15.00262158 |
| mean anomaly at epoch: | 259.4550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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