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 22178.68045035 .00000024 00000-0 10000-3 0 9998
2 32953 82.5029 177.5764 0018059 236.0838 123.8523 12.43111274639604
| Epoch (UTC): | 27 June 2022 16:19:50 |
| Eccentricity: | 0.0018059 |
| inclination: | 82.5029° |
| perigee height: | 1479 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 177.5764° |
| argument of perigee: | 236.0838° |
| revolutions per day: | 12.43111274 |
| mean anomaly at epoch: | 123.8523° |
| orbit number at epoch: | 63960 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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