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 23088.53329983 .00004776 00000-0 48082-3 0 9999
2 26548 64.5507 241.1632 0048041 282.2196 77.3536 14.91485806220292
| Epoch (UTC): | 29 March 2023 12:47:57 |
| Eccentricity: | 0.0048041 |
| inclination: | 64.5507° |
| perigee height: | 560 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 241.1632° |
| argument of perigee: | 282.2196° |
| revolutions per day: | 14.91485806 |
| mean anomaly at epoch: | 77.3536° |
| orbit number at epoch: | 22029 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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