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 05175U 26017.86597214 +.00000000 +00000-0 +66141-4 0 00001
2 05175 74.0464 193.8085 0029796 342.9630 17.0522 14.39436256 09
| Epoch (UTC): | 17 January 2026 20:46:59 |
| Eccentricity: | 0.0029796 |
| inclination: | 74.0464° |
| perigee height: | 739 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 193.8085° |
| argument of perigee: | 342.9630° |
| revolutions per day: | 14.39436256 |
| mean anomaly at epoch: | 17.0522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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