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 60235U 24128A 24357.83772809 .00005659 00000-0 50035-3 0 9999
2 60235 61.9966 308.9421 0034052 2.2039 357.9192 14.97004778 24832
| Epoch (UTC): | 22 December 2024 20:06:19 |
| Eccentricity: | 0.0034052 |
| inclination: | 61.9966° |
| perigee height: | 552 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 308.9421° |
| argument of perigee: | 2.2039° |
| revolutions per day: | 14.97004778 |
| mean anomaly at epoch: | 357.9192° |
| orbit number at epoch: | 2483 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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