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 27844U 03031E 22177.57081565 .00000172 00000-0 96635-4 0 9991
2 27844 98.6777 185.1193 0011133 77.4993 282.7430 14.22458864985166
| Epoch (UTC): | 26 June 2022 13:41:58 |
| Eccentricity: | 0.0011133 |
| inclination: | 98.6777° |
| perigee height: | 809 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 185.1193° |
| argument of perigee: | 77.4993° |
| revolutions per day: | 14.22458864 |
| mean anomaly at epoch: | 282.7430° |
| orbit number at epoch: | 98516 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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