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 15517U 85013B 23151.13142266 .00000045 00000-0 26971-4 0 9991
2 15517 82.5339 150.2171 0014225 201.5684 158.4879 13.84924045936389
| Epoch (UTC): | 31 May 2023 03:09:14 |
| Eccentricity: | 0.0014225 |
| inclination: | 82.5339° |
| perigee height: | 936 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 150.2171° |
| argument of perigee: | 201.5684° |
| revolutions per day: | 13.84924045 |
| mean anomaly at epoch: | 158.4879° |
| orbit number at epoch: | 93638 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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