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 22136.51023946 .00000249 00000-0 10186-3 0 9992
2 39090 98.4068 335.4780 0009368 14.5236 345.6217 14.35285012482817
| Epoch (UTC): | 16 May 2022 12:14:44 |
| Eccentricity: | 0.0009368 |
| inclination: | 98.4068° |
| perigee height: | 767 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 335.4780° |
| argument of perigee: | 14.5236° |
| revolutions per day: | 14.35285012 |
| mean anomaly at epoch: | 345.6217° |
| orbit number at epoch: | 48281 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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