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 26066.51494822 +.00000000 +00000-0 +94588-4 0 00004
2 05175 74.0463 104.0661 0030723 244.3877 115.4102 14.39474607 01
| Epoch (UTC): | 07 March 2026 12:21:31 |
| Eccentricity: | 0.0030723 |
| inclination: | 74.0463° |
| perigee height: | 738 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 104.0661° |
| argument of perigee: | 244.3877° |
| revolutions per day: | 14.39474607 |
| mean anomaly at epoch: | 115.4102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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