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 35935U 09051E 22179.13791284 .00000294 00000-0 77861-4 0 9994
2 35935 98.5719 37.0493 0008846 37.6380 322.5435 14.56000121677469
| Epoch (UTC): | 28 June 2022 03:18:35 |
| Eccentricity: | 0.0008846 |
| inclination: | 98.5719° |
| perigee height: | 700 km |
| apogee height: | 712 km |
| right ascension of ascending node: | 37.0493° |
| argument of perigee: | 37.6380° |
| revolutions per day: | 14.56000121 |
| mean anomaly at epoch: | 322.5435° |
| orbit number at epoch: | 67746 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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