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 61905U 24205M 24358.48335356 .00013159 00000-0 69616-3 0 9993
2 61905 97.4734 69.9539 0015665 136.8761 223.3701 15.15472317 6373
| Epoch (UTC): | 23 December 2024 11:36:01 |
| Eccentricity: | 0.0015665 |
| inclination: | 97.4734° |
| perigee height: | 509 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 69.9539° |
| argument of perigee: | 136.8761° |
| revolutions per day: | 15.15472317 |
| mean anomaly at epoch: | 223.3701° |
| orbit number at epoch: | 637 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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