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 09904U 26088.19058691 +.00000000 +00000-0 +11251-3 0 00001
2 09904 81.2593 270.3659 0053776 292.4330 67.1149 14.07315663 09
| Epoch (UTC): | 29 March 2026 04:34:26 |
| Eccentricity: | 0.0053776 |
| inclination: | 81.2593° |
| perigee height: | 830 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 270.3659° |
| argument of perigee: | 292.4330° |
| revolutions per day: | 14.07315663 |
| mean anomaly at epoch: | 67.1149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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