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 60262U 26145.17089969 +.00000000 +00000-0 +60775-4 0 00005
2 60262 53.1611 56.7987 0001219 86.2831 273.8310 15.31707004 00
| Epoch (UTC): | 25 May 2026 04:06:05 |
| Eccentricity: | 0.0001219 |
| inclination: | 53.1611° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 56.7987° |
| argument of perigee: | 86.2831° |
| revolutions per day: | 15.31707004 |
| mean anomaly at epoch: | 273.8310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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