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 22825U 93061C 23081.11345225 .00000193 00000-0 92253-4 0 9993
2 22825 98.8533 122.5529 0007765 328.4772 31.5944 14.30268428538113
| Epoch (UTC): | 22 March 2023 02:43:22 |
| Eccentricity: | 0.0007765 |
| inclination: | 98.8533° |
| perigee height: | 785 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 122.5529° |
| argument of perigee: | 328.4772° |
| revolutions per day: | 14.30268428 |
| mean anomaly at epoch: | 31.5944° |
| orbit number at epoch: | 53811 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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