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 57858U 26145.64957537 +.00000000 +00000-0 +65449-4 0 00002
2 57858 53.1630 286.4558 0001201 105.4983 254.6150 15.30199885 07
| Epoch (UTC): | 25 May 2026 15:35:23 |
| Eccentricity: | 0.0001201 |
| inclination: | 53.1630° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 286.4558° |
| argument of perigee: | 105.4983° |
| revolutions per day: | 15.30199885 |
| mean anomaly at epoch: | 254.6150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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