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 22141.89041244 .00000931 00000-0 22266-3 0 9996
2 35935 98.5760 358.7942 0008759 138.0361 222.1508 14.55962143672017
| Epoch (UTC): | 21 May 2022 21:22:11 |
| Eccentricity: | 0.0008759 |
| inclination: | 98.5760° |
| perigee height: | 700 km |
| apogee height: | 712 km |
| right ascension of ascending node: | 358.7942° |
| argument of perigee: | 138.0361° |
| revolutions per day: | 14.55962143 |
| mean anomaly at epoch: | 222.1508° |
| orbit number at epoch: | 67201 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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