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 42766U 17036B 24118.29613428 .08122670 23474-5 90128-3 0 9997
2 42766 97.0758 154.7708 0010233 252.0492 107.9692 16.37099332381647
| Epoch (UTC): | 27 April 2024 07:06:26 |
| Eccentricity: | 0.0010233 |
| inclination: | 97.0758° |
| perigee height: | 167 km |
| apogee height: | 180 km |
| right ascension of ascending node: | 154.7708° |
| argument of perigee: | 252.0492° |
| revolutions per day: | 16.37099332 |
| mean anomaly at epoch: | 107.9692° |
| orbit number at epoch: | 38164 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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