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 41049U 00055G 22226.15194915 .00001195 00000-0 64210-3 0 9999
2 41049 98.7391 291.6083 0005879 252.0935 107.9597 14.14777241346471
| Epoch (UTC): | 14 August 2022 03:38:48 |
| Eccentricity: | 0.0005879 |
| inclination: | 98.7391° |
| perigee height: | 839 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 291.6083° |
| argument of perigee: | 252.0935° |
| revolutions per day: | 14.14777241 |
| mean anomaly at epoch: | 107.9597° |
| orbit number at epoch: | 34647 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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