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 16369U 85116B 23153.55193329 .00000204 00000-0 19037-3 0 9996
2 16369 82.9361 169.6311 0036142 185.8651 287.9488 13.76956829881169
| Epoch (UTC): | 02 June 2023 13:14:47 |
| Eccentricity: | 0.0036142 |
| inclination: | 82.9361° |
| perigee height: | 948 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 169.6311° |
| argument of perigee: | 185.8651° |
| revolutions per day: | 13.76956829 |
| mean anomaly at epoch: | 287.9488° |
| orbit number at epoch: | 88116 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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