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 22176.34645405 .00000024 00000-0 10000-3 0 9996
2 32953 82.5031 179.0276 0018015 241.4788 118.4478 12.43111222639318
| Epoch (UTC): | 25 June 2022 08:18:53 |
| Eccentricity: | 0.0018015 |
| inclination: | 82.5031° |
| perigee height: | 1479 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 179.0276° |
| argument of perigee: | 241.4788° |
| revolutions per day: | 12.43111222 |
| mean anomaly at epoch: | 118.4478° |
| orbit number at epoch: | 63931 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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