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 48824U 61015NC 24357.96157630 .00000301 00000-0 23616-3 0 9992
2 48824 67.0019 196.2668 0096052 326.9818 32.5293 14.02452146567313
| Epoch (UTC): | 22 December 2024 23:04:40 |
| Eccentricity: | 0.0096052 |
| inclination: | 67.0019° |
| perigee height: | 815 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 196.2668° |
| argument of perigee: | 326.9818° |
| revolutions per day: | 14.02452146 |
| mean anomaly at epoch: | 32.5293° |
| orbit number at epoch: | 56731 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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