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 23035.88552079 .00037398 00000-0 72167-3 0 9995
2 39026 97.2815 30.5748 0025841 46.1733 314.1647 15.47358474564712
| Epoch (UTC): | 04 February 2023 21:15:08 |
| Eccentricity: | 0.0025841 |
| inclination: | 97.2815° |
| perigee height: | 407 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 30.5748° |
| argument of perigee: | 46.1733° |
| revolutions per day: | 15.47358474 |
| mean anomaly at epoch: | 314.1647° |
| orbit number at epoch: | 56471 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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