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 61076U 24140MS 24358.42764001 .00002804 00000-0 13395-2 0 9994
2 61076 89.0298 336.0086 0052016 130.9661 229.6047 14.18222090 17450
| Epoch (UTC): | 23 December 2024 10:15:48 |
| Eccentricity: | 0.0052016 |
| inclination: | 89.0298° |
| perigee height: | 794 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 336.0086° |
| argument of perigee: | 130.9661° |
| revolutions per day: | 14.18222090 |
| mean anomaly at epoch: | 229.6047° |
| orbit number at epoch: | 1745 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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