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 55764U 26145.42245133 +.00000000 +00000-0 -25087-4 0 00009
2 55764 69.9999 31.1211 0002747 267.9700 92.1144 14.98330252 08
| Epoch (UTC): | 25 May 2026 10:08:19 |
| Eccentricity: | 0.0002747 |
| inclination: | 69.9999° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 31.1211° |
| argument of perigee: | 267.9700° |
| revolutions per day: | 14.98330252 |
| mean anomaly at epoch: | 92.1144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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