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 44909U 19096E 23150.08405859 .00000019 00000-0 35706-4 0 9996
2 44909 82.5227 359.9779 0216581 229.1317 129.0840 12.79720788159843
| Epoch (UTC): | 30 May 2023 02:01:02 |
| Eccentricity: | 0.0216581 |
| inclination: | 82.5227° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 359.9779° |
| argument of perigee: | 229.1317° |
| revolutions per day: | 12.79720788 |
| mean anomaly at epoch: | 129.0840° |
| orbit number at epoch: | 15984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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