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 25791U 26088.19328663 +.00000000 +00000-0 +11068-3 0 00008
2 25791 24.9832 139.2221 0010000 324.7951 35.1896 14.44437348 00
| Epoch (UTC): | 29 March 2026 04:38:19 |
| Eccentricity: | 0.0010000 |
| inclination: | 24.9832° |
| perigee height: | 737 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 139.2221° |
| argument of perigee: | 324.7951° |
| revolutions per day: | 14.44437348 |
| mean anomaly at epoch: | 35.1896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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