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 15593U 85020B 23033.73611341 .00000533 00000-0 59944-4 0 9991
2 15593 82.5399 137.8538 0012997 86.9004 273.3699 14.84767878 49452
| Epoch (UTC): | 02 February 2023 17:40:00 |
| Eccentricity: | 0.0012997 |
| inclination: | 82.5399° |
| perigee height: | 605 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 137.8538° |
| argument of perigee: | 86.9004° |
| revolutions per day: | 14.84767878 |
| mean anomaly at epoch: | 273.3699° |
| orbit number at epoch: | 4945 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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