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 59U 60013B 23038.03711781 .00000161 00000-0 98572-4 0 9991
2 59 28.2484 303.2493 0189184 102.4080 259.7705 13.53017601 77842
| Epoch (UTC): | 07 February 2023 00:53:26 |
| Eccentricity: | 0.0189184 |
| inclination: | 28.2484° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 303.2493° |
| argument of perigee: | 102.4080° |
| revolutions per day: | 13.53017601 |
| mean anomaly at epoch: | 259.7705° |
| orbit number at epoch: | 7784 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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