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 22273.65931998 .00000030 00000-0 69145-4 0 9999
2 44909 82.5237 160.4005 0218389 73.7924 288.7087 12.79715275128966
| Epoch (UTC): | 30 September 2022 15:49:25 |
| Eccentricity: | 0.0218389 |
| inclination: | 82.5237° |
| perigee height: | 1174 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 160.4005° |
| argument of perigee: | 73.7924° |
| revolutions per day: | 12.79715275 |
| mean anomaly at epoch: | 288.7087° |
| orbit number at epoch: | 12896 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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