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 19257U 88053B 22221.63887135 .00000059 00000-0 28383-4 0 9990
2 19257 74.0498 0.7678 0019864 147.9610 340.9237 14.37618119788543
| Epoch (UTC): | 09 August 2022 15:19:58 |
| Eccentricity: | 0.0019864 |
| inclination: | 74.0498° |
| perigee height: | 752 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 0.7678° |
| argument of perigee: | 147.9610° |
| revolutions per day: | 14.37618119 |
| mean anomaly at epoch: | 340.9237° |
| orbit number at epoch: | 78854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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