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 35933U 09051C 23030.16024976 .00000885 00000-0 20655-3 0 9993
2 35933 98.5340 258.5775 0006903 83.6009 276.5975 14.57227530709268
| Epoch (UTC): | 30 January 2023 03:50:45 |
| Eccentricity: | 0.0006903 |
| inclination: | 98.5340° |
| perigee height: | 697 km |
| apogee height: | 707 km |
| right ascension of ascending node: | 258.5775° |
| argument of perigee: | 83.6009° |
| revolutions per day: | 14.57227530 |
| mean anomaly at epoch: | 276.5975° |
| orbit number at epoch: | 70926 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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