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 26071.17328442 +.00000000 +00000-0 +28747-3 0 00007
2 60235 61.9933 208.5724 0060261 113.1780 247.5674 15.00664867 01
| Epoch (UTC): | 12 March 2026 04:09:31 |
| Eccentricity: | 0.0060261 |
| inclination: | 61.9933° |
| perigee height: | 523 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 208.5724° |
| argument of perigee: | 113.1780° |
| revolutions per day: | 15.00664867 |
| mean anomaly at epoch: | 247.5674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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