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 18959U 88020B 23340.14757044 .00000602 00000-0 69005-4 0 9996
2 18959 82.5384 222.1994 0014953 261.8314 98.1205 14.84218797909835
| Epoch (UTC): | 06 December 2023 03:32:30 |
| Eccentricity: | 0.0014953 |
| inclination: | 82.5384° |
| perigee height: | 605 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 222.1994° |
| argument of perigee: | 261.8314° |
| revolutions per day: | 14.84218797 |
| mean anomaly at epoch: | 98.1205° |
| orbit number at epoch: | 90983 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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