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 26159.84778711 +.00000000 +00000-0 +20716-3 0 00004
2 60235 61.9936 260.2492 0051376 133.9260 226.6088 15.01115919 08
| Epoch (UTC): | 08 June 2026 20:20:48 |
| Eccentricity: | 0.0051376 |
| inclination: | 61.9936° |
| perigee height: | 528 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 260.2492° |
| argument of perigee: | 133.9260° |
| revolutions per day: | 15.01115919 |
| mean anomaly at epoch: | 226.6088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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