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 35869U 09049E 23273.49249484 .00000201 00000-0 10892-3 0 9990
2 35869 98.5934 234.7689 0003543 303.5301 56.5538 14.22671620728617
| Epoch (UTC): | 30 September 2023 11:49:11 |
| Eccentricity: | 0.0003543 |
| inclination: | 98.5934° |
| perigee height: | 814 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 234.7689° |
| argument of perigee: | 303.5301° |
| revolutions per day: | 14.22671620 |
| mean anomaly at epoch: | 56.5538° |
| orbit number at epoch: | 72861 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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