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 23154.54068454 .00000868 00000-0 14588-3 0 9993
2 16613 98.7505 2.1662 0141111 127.4860 233.9270 14.66186852648109
| Epoch (UTC): | 03 June 2023 12:58:35 |
| Eccentricity: | 0.0141111 |
| inclination: | 98.7505° |
| perigee height: | 574 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 2.1662° |
| argument of perigee: | 127.4860° |
| revolutions per day: | 14.66186852 |
| mean anomaly at epoch: | 233.9270° |
| orbit number at epoch: | 64810 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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