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 26110.94985813 +.00000000 +00000-0 +12666-3 0 00000
2 60235 61.9938 70.2906 0056861 122.2741 238.3876 15.00866281 07
| Epoch (UTC): | 20 April 2026 22:47:47 |
| Eccentricity: | 0.0056861 |
| inclination: | 61.9938° |
| perigee height: | 525 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 70.2906° |
| argument of perigee: | 122.2741° |
| revolutions per day: | 15.00866281 |
| mean anomaly at epoch: | 238.3876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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