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 23159.54421025 .00000011 00000-0 50366-6 0 9992
2 44909 82.5218 353.6902 0216920 206.9389 152.0319 12.79720981161059
| Epoch (UTC): | 08 June 2023 13:03:39 |
| Eccentricity: | 0.0216920 |
| inclination: | 82.5218° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 353.6902° |
| argument of perigee: | 206.9389° |
| revolutions per day: | 12.79720981 |
| mean anomaly at epoch: | 152.0319° |
| orbit number at epoch: | 16105 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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