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 56776U 26145.36102764 +.00000000 +00000-0 +54320-4 0 00009
2 56776 69.9987 131.3235 0003602 267.5831 92.4916 14.98329478 08
| Epoch (UTC): | 25 May 2026 08:39:52 |
| Eccentricity: | 0.0003602 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 131.3235° |
| argument of perigee: | 267.5831° |
| revolutions per day: | 14.98329478 |
| mean anomaly at epoch: | 92.4916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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