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 43937U 19003F 22175.81750786 .00008623 00000-0 28941-3 0 9994
2 43937 97.1299 208.8817 0022428 125.3822 234.9519 15.30854355191104
| Epoch (UTC): | 24 June 2022 19:37:12 |
| Eccentricity: | 0.0022428 |
| inclination: | 97.1299° |
| perigee height: | 458 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 208.8817° |
| argument of perigee: | 125.3822° |
| revolutions per day: | 15.30854355 |
| mean anomaly at epoch: | 234.9519° |
| orbit number at epoch: | 19110 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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