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 23150.56479314 .00000125 00000-0 51607-4 0 9991
2 16682 74.0247 194.3894 0014707 359.9733 161.8734 14.36274471942829
| Epoch (UTC): | 30 May 2023 13:33:18 |
| Eccentricity: | 0.0014707 |
| inclination: | 74.0247° |
| perigee height: | 760 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 194.3894° |
| argument of perigee: | 359.9733° |
| revolutions per day: | 14.36274471 |
| mean anomaly at epoch: | 161.8734° |
| orbit number at epoch: | 94282 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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