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 39090U 13009E 21015.79332925 .00000028 00000-0 24920-4 0 9994
2 39090 98.4367 221.4814 0009497 19.6841 340.4709 14.35163933413148
| Epoch (UTC): | 15 January 2021 19:02:23 |
| Eccentricity: | 0.0009497 |
| inclination: | 98.4367° |
| perigee height: | 768 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 221.4814° |
| argument of perigee: | 19.6841° |
| revolutions per day: | 14.35163933 |
| mean anomaly at epoch: | 340.4709° |
| orbit number at epoch: | 41314 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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