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 18616U 69082LB 24275.86380540 .00001821 00000-0 14359-2 0 9997
2 18616 70.1361 79.3155 0169510 356.1896 3.7901 13.86644417858052
| Epoch (UTC): | 01 October 2024 20:43:52 |
| Eccentricity: | 0.0169510 |
| inclination: | 70.1361° |
| perigee height: | 816 km |
| apogee height: | 1064 km |
| right ascension of ascending node: | 79.3155° |
| argument of perigee: | 356.1896° |
| revolutions per day: | 13.86644417 |
| mean anomaly at epoch: | 3.7901° |
| orbit number at epoch: | 85805 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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