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 17291U 26075.96623606 +.00000000 +00000-0 +11565-4 0 00003
2 17291 82.4714 174.7605 0012548 88.2013 272.0585 13.84688475 03
| Epoch (UTC): | 16 March 2026 23:11:22 |
| Eccentricity: | 0.0012548 |
| inclination: | 82.4714° |
| perigee height: | 938 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 174.7605° |
| argument of perigee: | 88.2013° |
| revolutions per day: | 13.84688475 |
| mean anomaly at epoch: | 272.0585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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