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 23029.54700885 .00034353 00000-0 67350-3 0 9997
2 39026 97.2817 24.2010 0026802 66.8432 293.5638 15.46889054563798
| Epoch (UTC): | 29 January 2023 13:07:41 |
| Eccentricity: | 0.0026802 |
| inclination: | 97.2817° |
| perigee height: | 407 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 24.2010° |
| argument of perigee: | 66.8432° |
| revolutions per day: | 15.46889054 |
| mean anomaly at epoch: | 293.5638° |
| orbit number at epoch: | 56379 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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