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 23159.50003461 .00000343 00000-0 13362-3 0 9991
2 39090 98.3889 353.1000 0007788 294.1726 65.8645 14.35598544538492
| Epoch (UTC): | 08 June 2023 12:00:02 |
| Eccentricity: | 0.0007788 |
| inclination: | 98.3889° |
| perigee height: | 767 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 353.1000° |
| argument of perigee: | 294.1726° |
| revolutions per day: | 14.35598544 |
| mean anomaly at epoch: | 65.8645° |
| orbit number at epoch: | 53849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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