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 23265.85815123 .00000616 00000-0 19843-3 0 9998
2 16864 74.0306 178.7558 0031512 74.5523 285.9109 14.41083097952249
| Epoch (UTC): | 22 September 2023 20:35:44 |
| Eccentricity: | 0.0031512 |
| inclination: | 74.0306° |
| perigee height: | 732 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 178.7558° |
| argument of perigee: | 74.5523° |
| revolutions per day: | 14.41083097 |
| mean anomaly at epoch: | 285.9109° |
| orbit number at epoch: | 95224 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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