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 26064.76653524 +.00000000 +00000-0 +73397-4 0 00002
2 17192 82.5080 145.8544 0017127 42.2121 79.8878 14.85909606 01
| Epoch (UTC): | 05 March 2026 18:23:48 |
| Eccentricity: | 0.0017127 |
| inclination: | 82.5080° |
| perigee height: | 599 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 145.8544° |
| argument of perigee: | 42.2121° |
| revolutions per day: | 14.85909606 |
| mean anomaly at epoch: | 79.8878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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