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 38293U 10059C 23337.43386801 .00000252 00000-0 11739-3 0 9994
2 38293 98.6894 49.4375 0012583 105.0936 255.1638 14.28924126675407
| Epoch (UTC): | 03 December 2023 10:24:46 |
| Eccentricity: | 0.0012583 |
| inclination: | 98.6894° |
| perigee height: | 786 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 49.4375° |
| argument of perigee: | 105.0936° |
| revolutions per day: | 14.28924126 |
| mean anomaly at epoch: | 255.1638° |
| orbit number at epoch: | 67540 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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