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 22026.93792422 .00007869 00000-0 25029-3 0 9993
2 39026 97.2607 19.8416 0031941 309.0020 50.8378 15.32370044507220
| Epoch (UTC): | 26 January 2022 22:30:36 |
| Eccentricity: | 0.0031941 |
| inclination: | 97.2607° |
| perigee height: | 447 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 19.8416° |
| argument of perigee: | 309.0020° |
| revolutions per day: | 15.32370044 |
| mean anomaly at epoch: | 50.8378° |
| orbit number at epoch: | 50722 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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