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 26076.30392021 +.00000000 +00000-0 +19942-3 0 00008
2 60235 61.9940 190.7391 0059857 114.3404 246.3952 15.00700220 06
| Epoch (UTC): | 17 March 2026 07:17:38 |
| Eccentricity: | 0.0059857 |
| inclination: | 61.9940° |
| perigee height: | 523 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 190.7391° |
| argument of perigee: | 114.3404° |
| revolutions per day: | 15.00700220 |
| mean anomaly at epoch: | 246.3952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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