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 23151.10043605 .00000032 00000-0 86878-4 0 9998
2 44909 82.5226 359.3024 0216614 226.7460 131.5386 12.79720811160020
| Epoch (UTC): | 31 May 2023 02:24:37 |
| Eccentricity: | 0.0216614 |
| inclination: | 82.5226° |
| perigee height: | 1175 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 359.3024° |
| argument of perigee: | 226.7460° |
| revolutions per day: | 12.79720811 |
| mean anomaly at epoch: | 131.5386° |
| orbit number at epoch: | 16002 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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