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 115U 60002D 22146.11650865 .00001575 00000-0 21031-3 0 9990
2 115 48.1642 110.1288 0033452 129.1651 231.2242 14.84349148318067
| Epoch (UTC): | 26 May 2022 02:47:46 |
| Eccentricity: | 0.0033452 |
| inclination: | 48.1642° |
| perigee height: | 592 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 110.1288° |
| argument of perigee: | 129.1651° |
| revolutions per day: | 14.84349148 |
| mean anomaly at epoch: | 231.2242° |
| orbit number at epoch: | 31806 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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