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 22268.51710286 .00000116 00000-0 59111-4 0 9994
2 20441 98.8308 240.5001 0010378 246.9653 228.1481 14.32980475707110
| Epoch (UTC): | 25 September 2022 12:24:37 |
| Eccentricity: | 0.0010378 |
| inclination: | 98.8308° |
| perigee height: | 774 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 240.5001° |
| argument of perigee: | 246.9653° |
| revolutions per day: | 14.32980475 |
| mean anomaly at epoch: | 228.1481° |
| orbit number at epoch: | 70711 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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