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 19922U 89028B 25199.04931093 -.00000010 00000-0 -24712-4 0 9998
2 19922 82.9564 35.9609 0035100 253.0155 106.7155 13.77465641823687
| Epoch (UTC): | 18 July 2025 01:11:00 |
| Eccentricity: | 0.0035100 |
| inclination: | 82.9564° |
| perigee height: | 947 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 35.9609° |
| argument of perigee: | 253.0155° |
| revolutions per day: | 13.77465641 |
| mean anomaly at epoch: | 106.7155° |
| orbit number at epoch: | 82368 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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