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 29842U 99025EL 23334.69112729 .00008622 00000-0 21147-2 0 9997
2 29842 98.6324 31.5880 0131727 274.7844 209.3214 14.47497334885683
| Epoch (UTC): | 30 November 2023 16:35:13 |
| Eccentricity: | 0.0131727 |
| inclination: | 98.6324° |
| perigee height: | 640 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 31.5880° |
| argument of perigee: | 274.7844° |
| revolutions per day: | 14.47497334 |
| mean anomaly at epoch: | 209.3214° |
| orbit number at epoch: | 88568 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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