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 24284.55640373 .00000087 00000-0 63951-4 0 9992
2 15517 82.5319 113.2243 0013578 243.9451 116.0313 13.84962471 4922
| Epoch (UTC): | 10 October 2024 13:21:13 |
| Eccentricity: | 0.0013578 |
| inclination: | 82.5319° |
| perigee height: | 936 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 113.2243° |
| argument of perigee: | 243.9451° |
| revolutions per day: | 13.84962471 |
| mean anomaly at epoch: | 116.0313° |
| orbit number at epoch: | 492 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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