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 41937U 17004A 23088.53035491 -.00000152 00000-0 00000-0 0 9996
2 41937 1.8409 327.8118 0002539 25.8433 287.1388 1.00274293 22810
| Epoch (UTC): | 29 March 2023 12:43:42 |
| Eccentricity: | 0.0002539 |
| inclination: | 1.8409° |
| perigee height: | 35775 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 327.8118° |
| argument of perigee: | 25.8433° |
| revolutions per day: | 1.00274293 |
| mean anomaly at epoch: | 287.1388° |
| orbit number at epoch: | 2281 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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