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 22183.78786837 .00000970 00000-0 52667-3 0 9993
2 41049 98.7397 250.1279 0007356 45.6966 314.4810 14.14667524340486
| Epoch (UTC): | 02 July 2022 18:54:31 |
| Eccentricity: | 0.0007356 |
| inclination: | 98.7397° |
| perigee height: | 838 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 250.1279° |
| argument of perigee: | 45.6966° |
| revolutions per day: | 14.14667524 |
| mean anomaly at epoch: | 314.4810° |
| orbit number at epoch: | 34048 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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