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 14506U 83113A 23152.46416756 .00000310 00000-0 14026-3 0 9994
2 14506 98.2978 327.7947 0009814 276.4774 137.3918 14.28515656 56690
| Epoch (UTC): | 01 June 2023 11:08:24 |
| Eccentricity: | 0.0009814 |
| inclination: | 98.2978° |
| perigee height: | 789 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 327.7947° |
| argument of perigee: | 276.4774° |
| revolutions per day: | 14.28515656 |
| mean anomaly at epoch: | 137.3918° |
| orbit number at epoch: | 5669 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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