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 26088.19112853 +.00000000 +00000-0 +58163-4 0 00004
2 17192 82.5038 123.7865 0015195 325.1037 105.0254 14.85931218 01
| Epoch (UTC): | 29 March 2026 04:35:13 |
| Eccentricity: | 0.0015195 |
| inclination: | 82.5038° |
| perigee height: | 600 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 123.7865° |
| argument of perigee: | 325.1037° |
| revolutions per day: | 14.85931218 |
| mean anomaly at epoch: | 105.0254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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