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 22178.51941972 .00000331 00000-0 86293-4 0 9997
2 35935 98.5720 36.4142 0008876 39.3333 320.8507 14.55999794677345
| Epoch (UTC): | 27 June 2022 12:27:57 |
| Eccentricity: | 0.0008876 |
| inclination: | 98.5720° |
| perigee height: | 700 km |
| apogee height: | 712 km |
| right ascension of ascending node: | 36.4142° |
| argument of perigee: | 39.3333° |
| revolutions per day: | 14.55999794 |
| mean anomaly at epoch: | 320.8507° |
| orbit number at epoch: | 67734 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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