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 23151.10222258 .00000208 00000-0 72760-4 0 9996
2 16864 74.0308 31.2406 0033373 314.0939 45.7470 14.40991138935973
| Epoch (UTC): | 31 May 2023 02:27:12 |
| Eccentricity: | 0.0033373 |
| inclination: | 74.0308° |
| perigee height: | 731 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 31.2406° |
| argument of perigee: | 314.0939° |
| revolutions per day: | 14.40991138 |
| mean anomaly at epoch: | 45.7470° |
| orbit number at epoch: | 93597 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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