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 24797U 97020F 25189.21113519 .00000667 00000-0 13126-3 0 9990
2 24797 86.8956 354.2713 0214847 212.8722 321.5577 14.47327667482863
| Epoch (UTC): | 08 July 2025 05:04:02 |
| Eccentricity: | 0.0214847 |
| inclination: | 86.8956° |
| perigee height: | 581 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 354.2713° |
| argument of perigee: | 212.8722° |
| revolutions per day: | 14.47327667 |
| mean anomaly at epoch: | 321.5577° |
| orbit number at epoch: | 48286 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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