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 29110U 06016D 22221.81345771 .00002932 00000-0 41732-3 0 9997
2 29110 98.4184 27.1583 0001933 251.2626 219.9851 14.77673272873363
| Epoch (UTC): | 09 August 2022 19:31:22 |
| Eccentricity: | 0.0001933 |
| inclination: | 98.4184° |
| perigee height: | 635 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 27.1583° |
| argument of perigee: | 251.2626° |
| revolutions per day: | 14.77673272 |
| mean anomaly at epoch: | 219.9851° |
| orbit number at epoch: | 87336 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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