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 17129U 26087.99596373 +.00000000 +00000-0 +11108-3 0 00001
2 17129 98.3096 102.5169 0033639 63.5509 357.9497 14.26065058 04
| Epoch (UTC): | 28 March 2026 23:54:11 |
| Eccentricity: | 0.0033639 |
| inclination: | 98.3096° |
| perigee height: | 781 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 102.5169° |
| argument of perigee: | 63.5509° |
| revolutions per day: | 14.26065058 |
| mean anomaly at epoch: | 357.9497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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