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 107U 61013A 24256.75142547 .00011042 00000-0 13897-2 0 9991
2 107 28.7918 47.3066 0516066 270.0382 84.1081 14.16633965184668
| Epoch (UTC): | 12 September 2024 18:02:03 |
| Eccentricity: | 0.0516066 |
| inclination: | 28.7918° |
| perigee height: | 464 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 47.3066° |
| argument of perigee: | 270.0382° |
| revolutions per day: | 14.16633965 |
| mean anomaly at epoch: | 84.1081° |
| orbit number at epoch: | 18466 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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