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 26107.95178690 +.00000000 +00000-0 +12009-3 0 00005
2 60235 61.9934 80.7149 0057135 121.5850 239.0835 15.00857232 05
| Epoch (UTC): | 17 April 2026 22:50:34 |
| Eccentricity: | 0.0057135 |
| inclination: | 61.9934° |
| perigee height: | 525 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 80.7149° |
| argument of perigee: | 121.5850° |
| revolutions per day: | 15.00857232 |
| mean anomaly at epoch: | 239.0835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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