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 08968U 75004BA 24357.57603543 .00001196 00000-0 45961-3 0 9996
2 08968 97.6210 16.8094 0131176 280.4422 78.2002 14.27364636531085
| Epoch (UTC): | 22 December 2024 13:49:29 |
| Eccentricity: | 0.0131176 |
| inclination: | 97.6210° |
| perigee height: | 706 km |
| apogee height: | 895 km |
| right ascension of ascending node: | 16.8094° |
| argument of perigee: | 280.4422° |
| revolutions per day: | 14.27364636 |
| mean anomaly at epoch: | 78.2002° |
| orbit number at epoch: | 53108 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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