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 26065.84260440 +.00000000 +00000-0 +37728-3 0 00006
2 60235 61.9930 227.0999 0060731 112.0404 248.7151 15.00617288 09
| Epoch (UTC): | 06 March 2026 20:13:21 |
| Eccentricity: | 0.0060731 |
| inclination: | 61.9930° |
| perigee height: | 523 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 227.0999° |
| argument of perigee: | 112.0404° |
| revolutions per day: | 15.00617288 |
| mean anomaly at epoch: | 248.7151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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