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 26022.45783484 +.00000000 +00000-0 +10937-3 0 00001
2 17192 82.5058 185.6963 0016338 172.8683 212.3013 14.85850953 04
| Epoch (UTC): | 22 January 2026 10:59:16 |
| Eccentricity: | 0.0016338 |
| inclination: | 82.5058° |
| perigee height: | 599 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 185.6963° |
| argument of perigee: | 172.8683° |
| revolutions per day: | 14.85850953 |
| mean anomaly at epoch: | 212.3013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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