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 22176.93775075 .00000179 00000-0 99710-4 0 9990
2 27844 98.6777 184.4958 0011139 79.1484 281.0947 14.22458556985070
| Epoch (UTC): | 25 June 2022 22:30:21 |
| Eccentricity: | 0.0011139 |
| inclination: | 98.6777° |
| perigee height: | 809 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 184.4958° |
| argument of perigee: | 79.1484° |
| revolutions per day: | 14.22458556 |
| mean anomaly at epoch: | 281.0947° |
| orbit number at epoch: | 98507 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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