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 37153U 10043B 23088.50399779 .00000015 00000-0 37876-4 0 9998
2 37153 82.4527 90.7604 0008735 113.5541 246.6454 12.40753493568635
| Epoch (UTC): | 29 March 2023 12:05:45 |
| Eccentricity: | 0.0008735 |
| inclination: | 82.4527° |
| perigee height: | 1496 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 90.7604° |
| argument of perigee: | 113.5541° |
| revolutions per day: | 12.40753493 |
| mean anomaly at epoch: | 246.6454° |
| orbit number at epoch: | 56863 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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