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 26092U 00004K 23083.58290258 .00003103 00000-0 90724-3 0 9990
2 26092 100.1855 215.4320 0032840 288.3839 71.3775 14.44627281215643
| Epoch (UTC): | 24 March 2023 13:59:22 |
| Eccentricity: | 0.0032840 |
| inclination: | 100.1855° |
| perigee height: | 720 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 215.4320° |
| argument of perigee: | 288.3839° |
| revolutions per day: | 14.44627281 |
| mean anomaly at epoch: | 71.3775° |
| orbit number at epoch: | 21564 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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