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 23151.92613912 .00000040 00000-0 22720-4 0 9992
2 15517 82.5339 149.5841 0014272 199.2653 160.7969 13.84924062936054
| Epoch (UTC): | 31 May 2023 22:13:38 |
| Eccentricity: | 0.0014272 |
| inclination: | 82.5339° |
| perigee height: | 936 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 149.5841° |
| argument of perigee: | 199.2653° |
| revolutions per day: | 13.84924062 |
| mean anomaly at epoch: | 160.7969° |
| orbit number at epoch: | 93605 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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