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 39161U 13021C 24262.70903195 .00004613 00000-0 65672-3 0 9990
2 39161 97.8201 326.3313 0007491 288.5827 71.4569 14.77283085610937
| Epoch (UTC): | 18 September 2024 17:01:00 |
| Eccentricity: | 0.0007491 |
| inclination: | 97.8201° |
| perigee height: | 632 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 326.3313° |
| argument of perigee: | 288.5827° |
| revolutions per day: | 14.77283085 |
| mean anomaly at epoch: | 71.4569° |
| orbit number at epoch: | 61093 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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