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 11289U 79021B 23266.01043655 .00000137 00000-0 66571-4 0 9993
2 11289 81.2431 90.9707 0074993 217.9240 141.6637 14.11757577293749
| Epoch (UTC): | 23 September 2023 00:15:01 |
| Eccentricity: | 0.0074993 |
| inclination: | 81.2431° |
| perigee height: | 799 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 90.9707° |
| argument of perigee: | 217.9240° |
| revolutions per day: | 14.11757577 |
| mean anomaly at epoch: | 141.6637° |
| orbit number at epoch: | 29374 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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