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 60059U 26145.37446490 +.00000000 +00000-0 +10044-4 0 00001
2 60059 53.1589 173.3165 0000966 74.7676 285.3449 15.69695698 06
| Epoch (UTC): | 25 May 2026 08:59:13 |
| Eccentricity: | 0.0000966 |
| inclination: | 53.1589° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 173.3165° |
| argument of perigee: | 74.7676° |
| revolutions per day: | 15.69695698 |
| mean anomaly at epoch: | 285.3449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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