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 20465U 90010A 23150.47152982 .00002652 00000-0 20800-3 0 9994
2 20465 82.4864 315.8554 0015053 161.9899 198.1862 15.00502789789634
| Epoch (UTC): | 30 May 2023 11:19:00 |
| Eccentricity: | 0.0015053 |
| inclination: | 82.4864° |
| perigee height: | 555 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 315.8554° |
| argument of perigee: | 161.9899° |
| revolutions per day: | 15.00502789 |
| mean anomaly at epoch: | 198.1862° |
| orbit number at epoch: | 78963 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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