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 35943U 09054B 22267.86041241 .00000024 00000-0 00000+0 0 9992
2 35943 0.0394 101.2152 0003049 99.3163 175.8945 1.00271675 47617
| Epoch (UTC): | 24 September 2022 20:38:59 |
| Eccentricity: | 0.0003049 |
| inclination: | 0.0394° |
| perigee height: | 35773 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 101.2152° |
| argument of perigee: | 99.3163° |
| revolutions per day: | 1.00271675 |
| mean anomaly at epoch: | 175.8945° |
| orbit number at epoch: | 4761 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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