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 60310U 26145.25562826 +.00000000 +00000-0 +16919-4 0 00007
2 60310 53.1592 128.4863 0000970 86.8249 273.2880 15.69706192 08
| Epoch (UTC): | 25 May 2026 06:08:06 |
| Eccentricity: | 0.0000970 |
| inclination: | 53.1592° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 128.4863° |
| argument of perigee: | 86.8249° |
| revolutions per day: | 15.69706192 |
| mean anomaly at epoch: | 273.2880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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