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 16496U 86006B 23150.45084997 .00000510 00000-0 57209-4 0 9996
2 16496 82.5229 132.5696 0020775 94.5992 21.4190 14.84696660998606
| Epoch (UTC): | 30 May 2023 10:49:13 |
| Eccentricity: | 0.0020775 |
| inclination: | 82.5229° |
| perigee height: | 600 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 132.5696° |
| argument of perigee: | 94.5992° |
| revolutions per day: | 14.84696660 |
| mean anomaly at epoch: | 21.4190° |
| orbit number at epoch: | 99860 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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