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 00059U 60013B 23344.52231804 .00000151 00000-0 81962-4 0 9992
2 00059 28.2460 168.7512 0189036 155.0626 205.9187 13.53051122118511
| Epoch (UTC): | 10 December 2023 12:32:08 |
| Eccentricity: | 0.0189036 |
| inclination: | 28.2460° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 168.7512° |
| argument of perigee: | 155.0626° |
| revolutions per day: | 13.53051122 |
| mean anomaly at epoch: | 205.9187° |
| orbit number at epoch: | 11851 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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