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 26071.97287258 +.00000000 +00000-0 +30493-3 0 00005
2 60235 61.9933 205.7933 0060199 113.3622 247.3816 15.00671847 01
| Epoch (UTC): | 12 March 2026 23:20:56 |
| Eccentricity: | 0.0060199 |
| inclination: | 61.9933° |
| perigee height: | 523 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 205.7933° |
| argument of perigee: | 113.3622° |
| revolutions per day: | 15.00671847 |
| mean anomaly at epoch: | 247.3816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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