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 44475U 19049A 23028.55901434 .00000155 00000-0 00000-0 0 9994
2 44475 0.0822 261.7527 0000430 6.4522 91.7609 1.00269433 12816
| Epoch (UTC): | 28 January 2023 13:24:58 |
| Eccentricity: | 0.0000430 |
| inclination: | 0.0822° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 261.7527° |
| argument of perigee: | 6.4522° |
| revolutions per day: | 1.00269433 |
| mean anomaly at epoch: | 91.7609° |
| orbit number at epoch: | 1281 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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