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 22137.27707925 .00000234 00000-0 96589-4 0 9998
2 39090 98.4067 336.2251 0009317 12.3301 347.8111 14.35285292482942
| Epoch (UTC): | 17 May 2022 06:38:59 |
| Eccentricity: | 0.0009317 |
| inclination: | 98.4067° |
| perigee height: | 767 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 336.2251° |
| argument of perigee: | 12.3301° |
| revolutions per day: | 14.35285292 |
| mean anomaly at epoch: | 347.8111° |
| orbit number at epoch: | 48294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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