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 05679U 71110B 23277.37995758 .00000072 00000-0 10792-3 0 9992
2 05679 69.9948 272.7616 0015411 296.0253 63.9260 13.85459644232668
| Epoch (UTC): | 04 October 2023 09:07:08 |
| Eccentricity: | 0.0015411 |
| inclination: | 69.9948° |
| perigee height: | 933 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 272.7616° |
| argument of perigee: | 296.0253° |
| revolutions per day: | 13.85459644 |
| mean anomaly at epoch: | 63.9260° |
| orbit number at epoch: | 23266 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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