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 59918U 24105B 24281.20367229 .00013925 00000-0 84153-3 0 9996
2 59918 97.6046 286.6514 0012364 200.0578 160.0167 15.10728320 19501
| Epoch (UTC): | 07 October 2024 04:53:17 |
| Eccentricity: | 0.0012364 |
| inclination: | 97.6046° |
| perigee height: | 525 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 286.6514° |
| argument of perigee: | 200.0578° |
| revolutions per day: | 15.10728320 |
| mean anomaly at epoch: | 160.0167° |
| orbit number at epoch: | 1950 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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