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 32788U 08021F 23160.49858498 .00010547 00000-0 77172-3 0 9990
2 32788 97.5591 140.0882 0008690 31.6767 328.4980 15.03742705821955
| Epoch (UTC): | 09 June 2023 11:57:57 |
| Eccentricity: | 0.0008690 |
| inclination: | 97.5591° |
| perigee height: | 549 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 140.0882° |
| argument of perigee: | 31.6767° |
| revolutions per day: | 15.03742705 |
| mean anomaly at epoch: | 328.4980° |
| orbit number at epoch: | 82195 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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