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 29522U 06050A 18315.71124904 0.00000020 00000-0 10536-4 0 01
2 29522 98.8401 329.9450 0011000 28.2704 331.7294 14.13991046 06
| Epoch (UTC): | 11 November 2018 17:04:11 |
| Eccentricity: | 0.0011000 |
| inclination: | 98.8401° |
| perigee height: | 838 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 329.9450° |
| argument of perigee: | 28.2704° |
| revolutions per day: | 14.13991046 |
| mean anomaly at epoch: | 331.7294° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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