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 60079U 26145.61508833 +.00000000 +00000-0 +10185-3 0 00005
2 60079 97.9834 169.9096 0003202 141.3994 218.7447 14.80580601 08
| Epoch (UTC): | 25 May 2026 14:45:43 |
| Eccentricity: | 0.0003202 |
| inclination: | 97.9834° |
| perigee height: | 625 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 169.9096° |
| argument of perigee: | 141.3994° |
| revolutions per day: | 14.80580601 |
| mean anomaly at epoch: | 218.7447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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