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 26075.77087250 +.00000000 +00000-0 +22098-3 0 00009
2 60235 61.9940 192.5919 0059891 114.2370 246.4994 15.00697456 04
| Epoch (UTC): | 16 March 2026 18:30:03 |
| Eccentricity: | 0.0059891 |
| inclination: | 61.9940° |
| perigee height: | 523 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 192.5919° |
| argument of perigee: | 114.2370° |
| revolutions per day: | 15.00697456 |
| mean anomaly at epoch: | 246.4994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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