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 22274.44113529 .00000033 00000-0 79707-4 0 9997
2 44909 82.5236 159.8816 0218419 71.9742 290.5026 12.79715380129062
| Epoch (UTC): | 01 October 2022 10:35:14 |
| Eccentricity: | 0.0218419 |
| inclination: | 82.5236° |
| perigee height: | 1174 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 159.8816° |
| argument of perigee: | 71.9742° |
| revolutions per day: | 12.79715380 |
| mean anomaly at epoch: | 290.5026° |
| orbit number at epoch: | 12906 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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