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 35685U 09041E 23267.81851060 .00002812 00000-0 31624-3 0 9992
2 35685 98.1159 346.1975 0056159 189.9178 170.0933 14.86411091766058
| Epoch (UTC): | 24 September 2023 19:38:39 |
| Eccentricity: | 0.0056159 |
| inclination: | 98.1159° |
| perigee height: | 570 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 346.1975° |
| argument of perigee: | 189.9178° |
| revolutions per day: | 14.86411091 |
| mean anomaly at epoch: | 170.0933° |
| orbit number at epoch: | 76605 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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