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 23155.61481733 .00000222 00000-0 76886-4 0 9990
2 16864 74.0303 22.8855 0033463 304.9064 54.8948 14.40993552936366
| Epoch (UTC): | 04 June 2023 14:45:20 |
| Eccentricity: | 0.0033463 |
| inclination: | 74.0303° |
| perigee height: | 731 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 22.8855° |
| argument of perigee: | 304.9064° |
| revolutions per day: | 14.40993552 |
| mean anomaly at epoch: | 54.8948° |
| orbit number at epoch: | 93636 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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