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 38341U 12025E 22139.49499892 .00002105 00000-0 24952-3 0 9993
2 38341 98.5085 352.8375 0055660 138.8916 221.6510 14.84657135541356
| Epoch (UTC): | 19 May 2022 11:52:47 |
| Eccentricity: | 0.0055660 |
| inclination: | 98.5085° |
| perigee height: | 576 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 352.8375° |
| argument of perigee: | 138.8916° |
| revolutions per day: | 14.84657135 |
| mean anomaly at epoch: | 221.6510° |
| orbit number at epoch: | 54135 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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