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 24258.93923884 .00004039 00000-0 86455-3 0 9992
2 35933 98.4495 144.8015 0006884 60.6465 299.5421 14.59294245795716
| Epoch (UTC): | 14 September 2024 22:32:30 |
| Eccentricity: | 0.0006884 |
| inclination: | 98.4495° |
| perigee height: | 690 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 144.8015° |
| argument of perigee: | 60.6465° |
| revolutions per day: | 14.59294245 |
| mean anomaly at epoch: | 299.5421° |
| orbit number at epoch: | 79571 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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