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 35240U 99025DQY 22222.14472287 .00001145 00000-0 66191-3 0 9991
2 35240 99.3424 111.2331 0058343 340.8603 19.0374 14.10292384758925
| Epoch (UTC): | 10 August 2022 03:28:24 |
| Eccentricity: | 0.0058343 |
| inclination: | 99.3424° |
| perigee height: | 816 km |
| apogee height: | 900 km |
| right ascension of ascending node: | 111.2331° |
| argument of perigee: | 340.8603° |
| revolutions per day: | 14.10292384 |
| mean anomaly at epoch: | 19.0374° |
| orbit number at epoch: | 75892 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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