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 60111U 26145.12411855 +.00000000 +00000-0 +57457-4 0 00009
2 60111 53.1611 41.7547 0001249 76.8769 283.2372 15.30193171 03
| Epoch (UTC): | 25 May 2026 02:58:43 |
| Eccentricity: | 0.0001249 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 41.7547° |
| argument of perigee: | 76.8769° |
| revolutions per day: | 15.30193171 |
| mean anomaly at epoch: | 283.2372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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