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 32953U 08025A 22177.47321083 .00000024 00000-0 10000-3 0 9994
2 32953 82.5031 178.3272 0018033 238.7824 121.1491 12.43111255639453
| Epoch (UTC): | 26 June 2022 11:21:25 |
| Eccentricity: | 0.0018033 |
| inclination: | 82.5031° |
| perigee height: | 1479 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 178.3272° |
| argument of perigee: | 238.7824° |
| revolutions per day: | 12.43111255 |
| mean anomaly at epoch: | 121.1491° |
| orbit number at epoch: | 63945 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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