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 20441U 90005F 23273.96421472 .00000323 00000-0 13441-3 0 9991
2 20441 98.8760 259.2196 0010397 240.5016 180.4366 14.33218174760402
| Epoch (UTC): | 30 September 2023 23:08:28 |
| Eccentricity: | 0.0010397 |
| inclination: | 98.8760° |
| perigee height: | 773 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 259.2196° |
| argument of perigee: | 240.5016° |
| revolutions per day: | 14.33218174 |
| mean anomaly at epoch: | 180.4366° |
| orbit number at epoch: | 76040 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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