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 42058U 17011A 23335.17122643 0.00000000 00000-0 00000-0 0 04
2 42058 63.4403 357.6418 0090005 2.6431 357.3569 13.40904698 07
| Epoch (UTC): | 01 December 2023 04:06:33 |
| Eccentricity: | 0.0090005 |
| inclination: | 63.4403° |
| perigee height: | 1038 km |
| apogee height: | 1173 km |
| right ascension of ascending node: | 357.6418° |
| argument of perigee: | 2.6431° |
| revolutions per day: | 13.40904698 |
| mean anomaly at epoch: | 357.3569° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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