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 23277.49377805 .00000700 00000-0 25696-3 0 9996
2 39090 98.3859 107.8574 0007967 303.2815 56.7607 14.35710686555409
| Epoch (UTC): | 04 October 2023 11:51:02 |
| Eccentricity: | 0.0007967 |
| inclination: | 98.3859° |
| perigee height: | 767 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 107.8574° |
| argument of perigee: | 303.2815° |
| revolutions per day: | 14.35710686 |
| mean anomaly at epoch: | 56.7607° |
| orbit number at epoch: | 55540 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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