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 42000U 17008BE 24193.14122659 .03664044 23375-5 67438-3 0 9994
2 42000 97.1246 256.7610 0012848 257.1819 102.8042 16.32105501412648
| Epoch (UTC): | 11 July 2024 03:23:21 |
| Eccentricity: | 0.0012848 |
| inclination: | 97.1246° |
| perigee height: | 178 km |
| apogee height: | 195 km |
| right ascension of ascending node: | 256.7610° |
| argument of perigee: | 257.1819° |
| revolutions per day: | 16.32105501 |
| mean anomaly at epoch: | 102.8042° |
| orbit number at epoch: | 41264 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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