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 26161.64631997 +.00000000 +00000-0 +16573-3 0 00005
2 60235 61.9942 253.9936 0051165 134.3542 226.1759 15.01123041 06
| Epoch (UTC): | 10 June 2026 15:30:42 |
| Eccentricity: | 0.0051165 |
| inclination: | 61.9942° |
| perigee height: | 528 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 253.9936° |
| argument of perigee: | 134.3542° |
| revolutions per day: | 15.01123041 |
| mean anomaly at epoch: | 226.1759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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