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 39026U 12072A 23147.45073076 .00067344 00000-0 70360-3 0 9994
2 39026 97.2799 144.1924 0013784 0.0866 0.0394 15.64152493582116
| Epoch (UTC): | 27 May 2023 10:49:03 |
| Eccentricity: | 0.0013784 |
| inclination: | 97.2799° |
| perigee height: | 366 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 144.1924° |
| argument of perigee: | 0.0866° |
| revolutions per day: | 15.64152493 |
| mean anomaly at epoch: | 0.0394° |
| orbit number at epoch: | 58211 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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