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 59U 60013B 23089.16731061 .00000137 00000-0 61434-4 0 9994
2 59 28.2498 40.5774 0189236 171.5458 188.8338 13.53024917 84776
| Epoch (UTC): | 30 March 2023 04:00:55 |
| Eccentricity: | 0.0189236 |
| inclination: | 28.2498° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 40.5774° |
| argument of perigee: | 171.5458° |
| revolutions per day: | 13.53024917 |
| mean anomaly at epoch: | 188.8338° |
| orbit number at epoch: | 8477 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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