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 31598U 07023A 22140.58749083 .00000302 00000-0 44447-4 0 9993
2 31598 97.8879 324.6519 0001429 95.0414 265.0963 14.82154173808839
| Epoch (UTC): | 20 May 2022 14:05:59 |
| Eccentricity: | 0.0001429 |
| inclination: | 97.8879° |
| perigee height: | 621 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 324.6519° |
| argument of perigee: | 95.0414° |
| revolutions per day: | 14.82154173 |
| mean anomaly at epoch: | 265.0963° |
| orbit number at epoch: | 80883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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