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 23260.74373246 0.00000000 00000-0 00000-0 0 01
2 42058 63.4403 187.0702 0083005 3.1498 356.8502 13.40902298 04
| Epoch (UTC): | 17 September 2023 17:50:58 |
| Eccentricity: | 0.0083005 |
| inclination: | 63.4403° |
| perigee height: | 1044 km |
| apogee height: | 1168 km |
| right ascension of ascending node: | 187.0702° |
| argument of perigee: | 3.1498° |
| revolutions per day: | 13.40902298 |
| mean anomaly at epoch: | 356.8502° |
| 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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