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 26548U 00057D 22222.09121544 .00000729 00000-0 90265-4 0 9997
2 26548 64.5490 245.9136 0035300 310.9939 48.8119 14.90280606186080
| Epoch (UTC): | 10 August 2022 02:11:21 |
| Eccentricity: | 0.0035300 |
| inclination: | 64.5490° |
| perigee height: | 572 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 245.9136° |
| argument of perigee: | 310.9939° |
| revolutions per day: | 14.90280606 |
| mean anomaly at epoch: | 48.8119° |
| orbit number at epoch: | 18608 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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