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 26064.21060978 +.00000000 +00000-0 +66480-4 0 00002
2 17192 82.5082 146.3780 0017174 44.0195 346.1232 14.85908662 09
| Epoch (UTC): | 05 March 2026 05:03:16 |
| Eccentricity: | 0.0017174 |
| inclination: | 82.5082° |
| perigee height: | 599 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 146.3780° |
| argument of perigee: | 44.0195° |
| revolutions per day: | 14.85908662 |
| mean anomaly at epoch: | 346.1232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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