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 22177.79514135 .00000024 00000-0 10000-3 0 9991
2 32953 82.5031 178.1268 0018047 238.0332 121.8997 12.43111270639497
| Epoch (UTC): | 26 June 2022 19:05:00 |
| Eccentricity: | 0.0018047 |
| inclination: | 82.5031° |
| perigee height: | 1479 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 178.1268° |
| argument of perigee: | 238.0332° |
| revolutions per day: | 12.43111270 |
| mean anomaly at epoch: | 121.8997° |
| orbit number at epoch: | 63949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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