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 16613U 86019A 23160.54619747 .00000934 00000-0 15615-3 0 9993
2 16613 98.7500 8.5655 0141242 108.9857 252.6710 14.66199141648989
| Epoch (UTC): | 09 June 2023 13:06:31 |
| Eccentricity: | 0.0141242 |
| inclination: | 98.7500° |
| perigee height: | 573 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 8.5655° |
| argument of perigee: | 108.9857° |
| revolutions per day: | 14.66199141 |
| mean anomaly at epoch: | 252.6710° |
| orbit number at epoch: | 64898 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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