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 23088U 94023B 23151.75656106 -.00000239 00000-0 -99104-4 0 9990
2 23088 71.0016 37.7321 0002753 351.1385 8.9689 14.14767655503086
| Epoch (UTC): | 31 May 2023 18:09:26 |
| Eccentricity: | 0.0002753 |
| inclination: | 71.0016° |
| perigee height: | 841 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 37.7321° |
| argument of perigee: | 351.1385° |
| revolutions per day: | 14.14767655 |
| mean anomaly at epoch: | 8.9689° |
| orbit number at epoch: | 50308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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