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 35865U 09049A 23332.85457686 .00000290 00000-0 14910-3 0 9990
2 35865 98.6052 293.5133 0003211 114.8308 245.3205 14.22591590736945
| Epoch (UTC): | 28 November 2023 20:30:35 |
| Eccentricity: | 0.0003211 |
| inclination: | 98.6052° |
| perigee height: | 814 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 293.5133° |
| argument of perigee: | 114.8308° |
| revolutions per day: | 14.22591590 |
| mean anomaly at epoch: | 245.3205° |
| orbit number at epoch: | 73694 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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