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 61426U 24140YT 24357.71609856 .00025433 00000-0 36545-2 0 9995
2 61426 89.1389 336.8934 0157495 312.2026 46.5908 14.68132046 17940
| Epoch (UTC): | 22 December 2024 17:11:10 |
| Eccentricity: | 0.0157495 |
| inclination: | 89.1389° |
| perigee height: | 556 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 336.8934° |
| argument of perigee: | 312.2026° |
| revolutions per day: | 14.68132046 |
| mean anomaly at epoch: | 46.5908° |
| orbit number at epoch: | 1794 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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