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 23150.93833276 .00002653 00000-0 20806-3 0 9994
2 20465 82.4864 315.4043 0015094 160.5726 199.6076 15.00505270810818
| Epoch (UTC): | 30 May 2023 22:31:11 |
| Eccentricity: | 0.0015094 |
| inclination: | 82.4864° |
| perigee height: | 555 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 315.4043° |
| argument of perigee: | 160.5726° |
| revolutions per day: | 15.00505270 |
| mean anomaly at epoch: | 199.6076° |
| orbit number at epoch: | 81081 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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