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 23083.44165656 .00005453 00000-0 83781-3 0 9997
2 39161 97.8794 158.1151 0008767 236.0879 123.9492 14.73915988530699
| Epoch (UTC): | 24 March 2023 10:35:59 |
| Eccentricity: | 0.0008767 |
| inclination: | 97.8794° |
| perigee height: | 642 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 158.1151° |
| argument of perigee: | 236.0879° |
| revolutions per day: | 14.73915988 |
| mean anomaly at epoch: | 123.9492° |
| orbit number at epoch: | 53069 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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