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 26088.16397639 +.00000000 +00000-0 +20289-3 0 00001
2 60235 61.9935 149.5128 0058828 116.9729 243.7386 15.00764599 06
| Epoch (UTC): | 29 March 2026 03:56:07 |
| Eccentricity: | 0.0058828 |
| inclination: | 61.9935° |
| perigee height: | 524 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 149.5128° |
| argument of perigee: | 116.9729° |
| revolutions per day: | 15.00764599 |
| mean anomaly at epoch: | 243.7386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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