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 30658U 99025APQ 23341.20442869 .00002082 00000-0 17228-2 0 9999
2 30658 98.4770 74.6452 0193531 84.8345 277.4865 13.81563424844924
| Epoch (UTC): | 07 December 2023 04:54:22 |
| Eccentricity: | 0.0193531 |
| inclination: | 98.4770° |
| perigee height: | 816 km |
| apogee height: | 1100 km |
| right ascension of ascending node: | 74.6452° |
| argument of perigee: | 84.8345° |
| revolutions per day: | 13.81563424 |
| mean anomaly at epoch: | 277.4865° |
| orbit number at epoch: | 84492 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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