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 35935U 09051E 23265.10662478 .00001366 00000-0 31527-3 0 9999
2 35935 98.5082 138.8418 0009261 85.5169 274.7086 14.56883787743076
| Epoch (UTC): | 22 September 2023 02:33:32 |
| Eccentricity: | 0.0009261 |
| inclination: | 98.5082° |
| perigee height: | 697 km |
| apogee height: | 710 km |
| right ascension of ascending node: | 138.8418° |
| argument of perigee: | 85.5169° |
| revolutions per day: | 14.56883787 |
| mean anomaly at epoch: | 274.7086° |
| orbit number at epoch: | 74307 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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