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 22568U 93014D 24357.78940900 .00004940 00000-0 13080-2 0 9999
2 22568 75.7478 256.8176 0149687 340.8551 72.1885 14.42433529656408
| Epoch (UTC): | 22 December 2024 18:56:44 |
| Eccentricity: | 0.0149687 |
| inclination: | 75.7478° |
| perigee height: | 644 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 256.8176° |
| argument of perigee: | 340.8551° |
| revolutions per day: | 14.42433529 |
| mean anomaly at epoch: | 72.1885° |
| orbit number at epoch: | 65640 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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