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 22177.53433435 .00000385 00000-0 96828-4 0 9990
2 35933 98.5621 35.3491 0006593 41.5933 318.5764 14.56890939677490
| Epoch (UTC): | 26 June 2022 12:49:26 |
| Eccentricity: | 0.0006593 |
| inclination: | 98.5621° |
| perigee height: | 698 km |
| apogee height: | 708 km |
| right ascension of ascending node: | 35.3491° |
| argument of perigee: | 41.5933° |
| revolutions per day: | 14.56890939 |
| mean anomaly at epoch: | 318.5764° |
| orbit number at epoch: | 67749 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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