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 22179.48527676 .00000024 00000-0 10000-3 0 9993
2 32953 82.5029 177.0758 0018064 234.3821 125.5578 12.43111315639707
| Epoch (UTC): | 28 June 2022 11:38:47 |
| Eccentricity: | 0.0018064 |
| inclination: | 82.5029° |
| perigee height: | 1479 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 177.0758° |
| argument of perigee: | 234.3821° |
| revolutions per day: | 12.43111315 |
| mean anomaly at epoch: | 125.5578° |
| orbit number at epoch: | 63970 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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