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 05560U 71089A 23028.35424992 .00000709 00000-0 18927-3 0 9990
2 05560 92.7162 144.7463 0014732 322.5459 37.4718 14.48492716697683
| Epoch (UTC): | 28 January 2023 08:30:07 |
| Eccentricity: | 0.0014732 |
| inclination: | 92.7162° |
| perigee height: | 720 km |
| apogee height: | 741 km |
| right ascension of ascending node: | 144.7463° |
| argument of perigee: | 322.5459° |
| revolutions per day: | 14.48492716 |
| mean anomaly at epoch: | 37.4718° |
| orbit number at epoch: | 69768 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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