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 59710U 26145.18714632 +.00000000 +00000-0 +84463-5 0 00005
2 59710 53.1605 309.4142 0001083 86.3472 273.7670 15.69709520 05
| Epoch (UTC): | 25 May 2026 04:29:29 |
| Eccentricity: | 0.0001083 |
| inclination: | 53.1605° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 309.4142° |
| argument of perigee: | 86.3472° |
| revolutions per day: | 15.69709520 |
| mean anomaly at epoch: | 273.7670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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