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 60066U 26145.34012803 +.00000000 +00000-0 -45320-5 0 00000
2 60066 53.1591 173.0862 0001157 94.4116 265.7034 15.69687714 01
| Epoch (UTC): | 25 May 2026 08:09:47 |
| Eccentricity: | 0.0001157 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 173.0862° |
| argument of perigee: | 94.4116° |
| revolutions per day: | 15.69687714 |
| mean anomaly at epoch: | 265.7034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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