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 60416U 26145.63903941 +.00000000 +00000-0 +54421-6 0 00005
2 60416 53.1606 235.0790 0001231 94.8729 265.2413 15.31696005 01
| Epoch (UTC): | 25 May 2026 15:20:13 |
| Eccentricity: | 0.0001231 |
| inclination: | 53.1606° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 235.0790° |
| argument of perigee: | 94.8729° |
| revolutions per day: | 15.31696005 |
| mean anomaly at epoch: | 265.2413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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