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 61085U 24140NB 24357.95123601 .00001175 00000-0 56126-3 0 9996
2 61085 89.1556 338.1948 0052173 139.8298 220.6766 14.17836800 16789
| Epoch (UTC): | 22 December 2024 22:49:46 |
| Eccentricity: | 0.0052173 |
| inclination: | 89.1556° |
| perigee height: | 795 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 338.1948° |
| argument of perigee: | 139.8298° |
| revolutions per day: | 14.17836800 |
| mean anomaly at epoch: | 220.6766° |
| orbit number at epoch: | 1678 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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