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 27432U 02024C 24261.63299097 .00000461 00000-0 26116-3 0 9996
2 27432 98.9670 304.3659 0051294 108.9757 2.4908 14.14370717153172
| Epoch (UTC): | 17 September 2024 15:11:30 |
| Eccentricity: | 0.0051294 |
| inclination: | 98.9670° |
| perigee height: | 807 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 304.3659° |
| argument of perigee: | 108.9757° |
| revolutions per day: | 14.14370717 |
| mean anomaly at epoch: | 2.4908° |
| orbit number at epoch: | 15317 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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