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 23154.08747825 .00000242 00000-0 83117-4 0 9994
2 16864 74.0304 25.7133 0033428 308.0080 51.8059 14.40992825936140
| Epoch (UTC): | 03 June 2023 02:05:58 |
| Eccentricity: | 0.0033428 |
| inclination: | 74.0304° |
| perigee height: | 731 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 25.7133° |
| argument of perigee: | 308.0080° |
| revolutions per day: | 14.40992825 |
| mean anomaly at epoch: | 51.8059° |
| orbit number at epoch: | 93614 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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