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 23149.87036837 .00000119 00000-0 49674-4 0 9996
2 16682 74.0247 195.6655 0014683 1.4774 171.2283 14.36274263942727
| Epoch (UTC): | 29 May 2023 20:53:19 |
| Eccentricity: | 0.0014683 |
| inclination: | 74.0247° |
| perigee height: | 760 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 195.6655° |
| argument of perigee: | 1.4774° |
| revolutions per day: | 14.36274263 |
| mean anomaly at epoch: | 171.2283° |
| orbit number at epoch: | 94272 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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