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 23151.93531750 .00000217 00000-0 75398-4 0 9997
2 16864 74.0307 29.6982 0033373 312.3923 47.4409 14.40991600935836
| Epoch (UTC): | 31 May 2023 22:26:51 |
| Eccentricity: | 0.0033373 |
| inclination: | 74.0307° |
| perigee height: | 731 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 29.6982° |
| argument of perigee: | 312.3923° |
| revolutions per day: | 14.40991600 |
| mean anomaly at epoch: | 47.4409° |
| orbit number at epoch: | 93583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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