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 26065.40298124 +.00000000 +00000-0 +96450-4 0 00008
2 05175 74.0463 106.1178 0030737 246.6267 113.1654 14.39473958 05
| Epoch (UTC): | 06 March 2026 09:40:17 |
| Eccentricity: | 0.0030737 |
| inclination: | 74.0463° |
| perigee height: | 738 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 106.1178° |
| argument of perigee: | 246.6267° |
| revolutions per day: | 14.39473958 |
| mean anomaly at epoch: | 113.1654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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