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 25940U 99057A 24281.40862411 .00001613 00000-0 56572-3 0 9992
2 25940 98.8183 263.4534 0005557 31.9716 328.1806 14.36447749308801
| Epoch (UTC): | 07 October 2024 09:48:25 |
| Eccentricity: | 0.0005557 |
| inclination: | 98.8183° |
| perigee height: | 766 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 263.4534° |
| argument of perigee: | 31.9716° |
| revolutions per day: | 14.36447749 |
| mean anomaly at epoch: | 328.1806° |
| orbit number at epoch: | 30880 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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