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 35660U 93036APB 22222.77500293 .00000561 00000-0 17207-3 0 9996
2 35660 74.0411 250.6895 0020383 336.0463 145.6791 14.43862798482307
| Epoch (UTC): | 10 August 2022 18:36:00 |
| Eccentricity: | 0.0020383 |
| inclination: | 74.0411° |
| perigee height: | 731 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 250.6895° |
| argument of perigee: | 336.0463° |
| revolutions per day: | 14.43862798 |
| mean anomaly at epoch: | 145.6791° |
| orbit number at epoch: | 48230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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