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 32789U 08021G 23090.53295747 .00073861 00000-0 26666-2 0 9999
2 32789 97.3139 112.9869 0008714 58.0108 302.1977 15.28169292815593
| Epoch (UTC): | 31 March 2023 12:47:27 |
| Eccentricity: | 0.0008714 |
| inclination: | 97.3139° |
| perigee height: | 475 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 112.9869° |
| argument of perigee: | 58.0108° |
| revolutions per day: | 15.28169292 |
| mean anomaly at epoch: | 302.1977° |
| orbit number at epoch: | 81559 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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