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 56927U 26145.37578098 +.00000000 +00000-0 -36314-4 0 00009
2 56927 43.0019 266.6665 0001264 268.4065 91.6642 15.27576513 09
| Epoch (UTC): | 25 May 2026 09:01:07 |
| Eccentricity: | 0.0001264 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.6665° |
| argument of perigee: | 268.4065° |
| revolutions per day: | 15.27576513 |
| mean anomaly at epoch: | 91.6642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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