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 22135.81311231 .00000263 00000-0 10687-3 0 9993
2 39090 98.4069 334.7989 0009414 16.5818 343.5674 14.35284725482714
| Epoch (UTC): | 15 May 2022 19:30:52 |
| Eccentricity: | 0.0009414 |
| inclination: | 98.4069° |
| perigee height: | 767 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 334.7989° |
| argument of perigee: | 16.5818° |
| revolutions per day: | 14.35284725 |
| mean anomaly at epoch: | 343.5674° |
| orbit number at epoch: | 48271 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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