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 16682U 86030B 23154.52428993 .00000158 00000-0 63003-4 0 9997
2 16682 74.0243 187.1130 0014869 351.8133 114.7433 14.36275945943700
| Epoch (UTC): | 03 June 2023 12:34:58 |
| Eccentricity: | 0.0014869 |
| inclination: | 74.0243° |
| perigee height: | 760 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 187.1130° |
| argument of perigee: | 351.8133° |
| revolutions per day: | 14.36275945 |
| mean anomaly at epoch: | 114.7433° |
| orbit number at epoch: | 94370 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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