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 23276.08871493 .00000016 00000-0 00000+0 0 9998
2 35943 0.0708 93.7191 0003348 123.8347 248.9269 1.00271782 51359
| Epoch (UTC): | 03 October 2023 02:07:44 |
| Eccentricity: | 0.0003348 |
| inclination: | 0.0708° |
| perigee height: | 35772 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 93.7191° |
| argument of perigee: | 123.8347° |
| revolutions per day: | 1.00271782 |
| mean anomaly at epoch: | 248.9269° |
| orbit number at epoch: | 5135 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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