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 26931U 01043C 23084.32439619 .00000616 00000-0 26589-3 0 9999
2 26931 67.0515 53.3544 0006968 282.8798 77.1525 14.30864877121586
| Epoch (UTC): | 25 March 2023 07:47:07 |
| Eccentricity: | 0.0006968 |
| inclination: | 67.0515° |
| perigee height: | 784 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 53.3544° |
| argument of perigee: | 282.8798° |
| revolutions per day: | 14.30864877 |
| mean anomaly at epoch: | 77.1525° |
| orbit number at epoch: | 12158 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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