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 23155.97196794 .00000027 00000-0 10430-4 0 9995
2 15517 82.5340 146.3616 0014538 187.5278 172.5667 13.84924317937059
| Epoch (UTC): | 04 June 2023 23:19:38 |
| Eccentricity: | 0.0014538 |
| inclination: | 82.5340° |
| perigee height: | 936 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 146.3616° |
| argument of perigee: | 187.5278° |
| revolutions per day: | 13.84924317 |
| mean anomaly at epoch: | 172.5667° |
| orbit number at epoch: | 93705 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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