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 26101.55584505 +.00000000 +00000-0 +13838-3 0 00002
2 60235 61.9925 102.9533 0057699 120.1075 240.5753 15.00838553 09
| Epoch (UTC): | 11 April 2026 13:20:25 |
| Eccentricity: | 0.0057699 |
| inclination: | 61.9925° |
| perigee height: | 524 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 102.9533° |
| argument of perigee: | 120.1075° |
| revolutions per day: | 15.00838553 |
| mean anomaly at epoch: | 240.5753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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