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 25159U 98007C 23027.28322351 .00001411 00000-0 58228-3 0 9991
2 25159 107.9789 152.7717 0044321 322.7961 37.0109 14.30722371299368
| Epoch (UTC): | 27 January 2023 06:47:50 |
| Eccentricity: | 0.0044321 |
| inclination: | 107.9789° |
| perigee height: | 757 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 152.7717° |
| argument of perigee: | 322.7961° |
| revolutions per day: | 14.30722371 |
| mean anomaly at epoch: | 37.0109° |
| orbit number at epoch: | 29936 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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