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 22334.55646490 .00018374 00000-0 41583-3 0 9992
2 39026 97.2798 324.1113 0023577 282.7323 77.1289 15.42888384554470
| Epoch (UTC): | 30 November 2022 13:21:18 |
| Eccentricity: | 0.0023577 |
| inclination: | 97.2798° |
| perigee height: | 421 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 324.1113° |
| argument of perigee: | 282.7323° |
| revolutions per day: | 15.42888384 |
| mean anomaly at epoch: | 77.1289° |
| orbit number at epoch: | 55447 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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