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 16864U 86052B 23160.89107344 .00000247 00000-0 84807-4 0 9998
2 16864 74.0300 13.1163 0033559 294.1501 65.6147 14.40996720937126
| Epoch (UTC): | 09 June 2023 21:23:08 |
| Eccentricity: | 0.0033559 |
| inclination: | 74.0300° |
| perigee height: | 731 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 13.1163° |
| argument of perigee: | 294.1501° |
| revolutions per day: | 14.40996720 |
| mean anomaly at epoch: | 65.6147° |
| orbit number at epoch: | 93712 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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