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 26109.48413704 +.00000000 +00000-0 +12719-3 0 00001
2 60235 61.9936 75.3869 0056997 121.9271 238.7380 15.00861875 01
| Epoch (UTC): | 19 April 2026 11:37:09 |
| Eccentricity: | 0.0056997 |
| inclination: | 61.9936° |
| perigee height: | 525 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 75.3869° |
| argument of perigee: | 121.9271° |
| revolutions per day: | 15.00861875 |
| mean anomaly at epoch: | 238.7380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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