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 data is extracted from the following two-line orbital elements,
1 05175U 71035B 23277.51863996 .00000459 00000-0 15824-3 0 9993
2 05175 74.0464 295.4869 0031053 293.4326 66.3564 14.38444131745334
| Epoch (UTC): | 04 October 2023 12:26:50 |
| Eccentricity: | 0.0031053 |
| inclination: | 74.0464° |
| perigee height: | 741 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 295.4869° |
| argument of perigee: | 293.4326° |
| revolutions per day: | 14.38444131 |
| mean anomaly at epoch: | 66.3564° |
| orbit number at epoch: | 74533 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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