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 41558U 16033C 23277.25834171 .16939764 26230-5 17999-3 0 9999
2 41558 97.4059 41.3631 0010829 262.8032 97.2042 16.50276834411181
| Epoch (UTC): | 04 October 2023 06:12:00 |
| Eccentricity: | 0.0010829 |
| inclination: | 97.4059° |
| perigee height: | 131 km |
| apogee height: | 145 km |
| right ascension of ascending node: | 41.3631° |
| argument of perigee: | 262.8032° |
| revolutions per day: | 16.50276834 |
| mean anomaly at epoch: | 97.2042° |
| orbit number at epoch: | 41118 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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