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 33505U 09003B 22227.31455314 .00001547 00000-0 91207-4 0 9999
2 33505 82.3904 168.0579 0024670 180.4107 179.7107 15.10616558745264
| Epoch (UTC): | 15 August 2022 07:32:57 |
| Eccentricity: | 0.0024670 |
| inclination: | 82.3904° |
| perigee height: | 517 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 168.0579° |
| argument of perigee: | 180.4107° |
| revolutions per day: | 15.10616558 |
| mean anomaly at epoch: | 179.7107° |
| orbit number at epoch: | 74526 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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