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 16615U 86019C 23151.73189001 .00000267 00000-0 11444-3 0 9996
2 16615 98.3271 199.5107 0013051 95.9947 13.6805 14.32184226950679
| Epoch (UTC): | 31 May 2023 17:33:55 |
| Eccentricity: | 0.0013051 |
| inclination: | 98.3271° |
| perigee height: | 775 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 199.5107° |
| argument of perigee: | 95.9947° |
| revolutions per day: | 14.32184226 |
| mean anomaly at epoch: | 13.6805° |
| orbit number at epoch: | 95067 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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