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 61252C 24175K 24349.51020833 .00007604 00000+0 62667-4 0 3495
2 61252 53.1558 115.7450 0001072 82.6093 46.0143 15.69688829 17
| Epoch (UTC): | 14 December 2024 12:14:42 |
| Eccentricity: | 0.0001072 |
| inclination: | 53.1558° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 115.7450° |
| argument of perigee: | 82.6093° |
| revolutions per day: | 15.69688829 |
| mean anomaly at epoch: | 46.0143° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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