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 9482U 76102B 22139.79601506 .00000076 00000-0 36049-4 0 9999
2 9482 81.2585 172.0341 0082303 135.3468 225.4369 14.07587203340676
| Epoch (UTC): | 19 May 2022 19:06:15 |
| Eccentricity: | 0.0082303 |
| inclination: | 81.2585° |
| perigee height: | 808 km |
| apogee height: | 927 km |
| right ascension of ascending node: | 172.0341° |
| argument of perigee: | 135.3468° |
| revolutions per day: | 14.07587203 |
| mean anomaly at epoch: | 225.4369° |
| orbit number at epoch: | 34067 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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