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 59899U 26145.15893028 +.00000000 +00000-0 +30610-4 0 00001
2 59899 43.0010 53.3831 0001078 267.3084 92.7645 15.27580865 09
| Epoch (UTC): | 25 May 2026 03:48:51 |
| Eccentricity: | 0.0001078 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 53.3831° |
| argument of perigee: | 267.3084° |
| revolutions per day: | 15.27580865 |
| mean anomaly at epoch: | 92.7645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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