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 20509U 90017B 23150.75811898 .00000183 00000-0 17313-3 0 9991
2 20509 82.9515 155.7345 0042270 209.8724 150.0019 13.75677137668839
| Epoch (UTC): | 30 May 2023 18:11:41 |
| Eccentricity: | 0.0042270 |
| inclination: | 82.9515° |
| perigee height: | 948 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 155.7345° |
| argument of perigee: | 209.8724° |
| revolutions per day: | 13.75677137 |
| mean anomaly at epoch: | 150.0019° |
| orbit number at epoch: | 66883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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