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 05707U 71114B 23083.66562455 .00000694 00000-0 23168-3 0 9990
2 05707 74.0279 159.0013 0023465 70.8900 289.4792 14.39234673685555
| Epoch (UTC): | 24 March 2023 15:58:29 |
| Eccentricity: | 0.0023465 |
| inclination: | 74.0279° |
| perigee height: | 744 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 159.0013° |
| argument of perigee: | 70.8900° |
| revolutions per day: | 14.39234673 |
| mean anomaly at epoch: | 289.4792° |
| orbit number at epoch: | 68555 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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