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 61906U 24205N 24358.13902057 .00022230 00000-0 11441-2 0 9996
2 61906 97.4723 69.6414 0015187 142.0480 218.1826 15.16334155 6320
| Epoch (UTC): | 23 December 2024 03:20:11 |
| Eccentricity: | 0.0015187 |
| inclination: | 97.4723° |
| perigee height: | 506 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 69.6414° |
| argument of perigee: | 142.0480° |
| revolutions per day: | 15.16334155 |
| mean anomaly at epoch: | 218.1826° |
| orbit number at epoch: | 632 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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