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 18986U 88023B 25193.78575372 -.00000015 00000-0 -29483-4 0 9995
2 18986 82.9538 10.2240 0040722 220.2846 139.5294 13.78890967876515
| Epoch (UTC): | 12 July 2025 18:51:29 |
| Eccentricity: | 0.0040722 |
| inclination: | 82.9538° |
| perigee height: | 938 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 10.2240° |
| argument of perigee: | 220.2846° |
| revolutions per day: | 13.78890967 |
| mean anomaly at epoch: | 139.5294° |
| orbit number at epoch: | 87651 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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