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 44355U 19036S 22110.24609159 .09797144 -77191-5 93620-3 0 9997
2 44355 28.5075 82.7172 0016307 255.7935 104.0877 16.36779689157079
| Epoch (UTC): | 20 April 2022 05:54:22 |
| Eccentricity: | 0.0016307 |
| inclination: | 28.5075° |
| perigee height: | 164 km |
| apogee height: | 185 km |
| right ascension of ascending node: | 82.7172° |
| argument of perigee: | 255.7935° |
| revolutions per day: | 16.36779689 |
| mean anomaly at epoch: | 104.0877° |
| orbit number at epoch: | 15707 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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