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 26049.91623133 +.00000000 +00000-0 +18539-3 0 00007
2 60235 61.9935 282.4513 0061892 108.4768 252.3062 15.00500094 00
| Epoch (UTC): | 18 February 2026 21:59:22 |
| Eccentricity: | 0.0061892 |
| inclination: | 61.9935° |
| perigee height: | 522 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 282.4513° |
| argument of perigee: | 108.4768° |
| revolutions per day: | 15.00500094 |
| mean anomaly at epoch: | 252.3062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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