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 25634U 99008A 24281.83099681 .00000570 00000-0 28887-3 0 9995
2 25634 98.4319 263.2295 0010887 36.0991 324.0919 14.19746030326696
| Epoch (UTC): | 07 October 2024 19:56:38 |
| Eccentricity: | 0.0010887 |
| inclination: | 98.4319° |
| perigee height: | 818 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 263.2295° |
| argument of perigee: | 36.0991° |
| revolutions per day: | 14.19746030 |
| mean anomaly at epoch: | 324.0919° |
| orbit number at epoch: | 32669 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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