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 29291U 79095Q 23002.35142386 .00007919 00000-0 26562-2 0 9991
2 29291 81.1848 237.4358 0016810 150.7637 209.4493 14.37111913854304
| Epoch (UTC): | 02 January 2023 08:26:03 |
| Eccentricity: | 0.0016810 |
| inclination: | 81.1848° |
| perigee height: | 756 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 237.4358° |
| argument of perigee: | 150.7637° |
| revolutions per day: | 14.37111913 |
| mean anomaly at epoch: | 209.4493° |
| orbit number at epoch: | 85430 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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