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 26112.28232742 +.00000000 +00000-0 +13821-3 0 00009
2 60235 61.9941 65.6577 0056746 122.5943 238.0644 15.00871450 06
| Epoch (UTC): | 22 April 2026 06:46:33 |
| Eccentricity: | 0.0056746 |
| inclination: | 61.9941° |
| perigee height: | 525 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 65.6577° |
| argument of perigee: | 122.5943° |
| revolutions per day: | 15.00871450 |
| mean anomaly at epoch: | 238.0644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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