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 17192U 26070.63243736 +.00000000 +00000-0 +58728-4 0 00006
2 17192 82.5072 140.3295 0016680 23.8566 137.2292 14.85916202 05
| Epoch (UTC): | 11 March 2026 15:10:42 |
| Eccentricity: | 0.0016680 |
| inclination: | 82.5072° |
| perigee height: | 599 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 140.3295° |
| argument of perigee: | 23.8566° |
| revolutions per day: | 14.85916202 |
| mean anomaly at epoch: | 137.2292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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