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 26020.15945524 +.00000000 +00000-0 +12993-3 0 00003
2 05175 74.0468 189.5778 0029886 338.2499 21.7384 14.39438625 05
| Epoch (UTC): | 20 January 2026 03:49:36 |
| Eccentricity: | 0.0029886 |
| inclination: | 74.0468° |
| perigee height: | 739 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 189.5778° |
| argument of perigee: | 338.2499° |
| revolutions per day: | 14.39438625 |
| mean anomaly at epoch: | 21.7384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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