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 26017.99339963 +.00000000 +00000-0 +15376-3 0 00001
2 60235 61.9947 33.3608 0063358 101.1017 259.7206 15.00254474 06
| Epoch (UTC): | 17 January 2026 23:50:29 |
| Eccentricity: | 0.0063358 |
| inclination: | 61.9947° |
| perigee height: | 522 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 33.3608° |
| argument of perigee: | 101.1017° |
| revolutions per day: | 15.00254474 |
| mean anomaly at epoch: | 259.7206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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