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 60411U 26145.31979894 +.00000000 +00000-0 +11150-4 0 00005
2 60411 53.1605 246.6078 0001114 94.6820 265.4308 15.31706131 09
| Epoch (UTC): | 25 May 2026 07:40:30 |
| Eccentricity: | 0.0001114 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 246.6078° |
| argument of perigee: | 94.6820° |
| revolutions per day: | 15.31706131 |
| mean anomaly at epoch: | 265.4308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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