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 26066.16745861 +.00000000 +00000-0 +79316-4 0 00009
2 05175 74.0463 104.7073 0030728 245.1108 114.6852 14.39474149 00
| Epoch (UTC): | 07 March 2026 04:01:08 |
| Eccentricity: | 0.0030728 |
| inclination: | 74.0463° |
| perigee height: | 738 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 104.7073° |
| argument of perigee: | 245.1108° |
| revolutions per day: | 14.39474149 |
| mean anomaly at epoch: | 114.6852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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