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 23331.58355247 .00001975 00000-0 44891-3 0 9992
2 35935 98.4979 206.6805 0006789 238.4749 121.5786 14.57108964752758
| Epoch (UTC): | 27 November 2023 14:00:18 |
| Eccentricity: | 0.0006789 |
| inclination: | 98.4979° |
| perigee height: | 698 km |
| apogee height: | 707 km |
| right ascension of ascending node: | 206.6805° |
| argument of perigee: | 238.4749° |
| revolutions per day: | 14.57108964 |
| mean anomaly at epoch: | 121.5786° |
| orbit number at epoch: | 75275 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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