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 23080.42480003 .00000020 00000-0 32083-4 0 9997
2 44909 82.5220 46.2515 0218190 32.4234 329.0058 12.79719280150930
| Epoch (UTC): | 21 March 2023 10:11:42 |
| Eccentricity: | 0.0218190 |
| inclination: | 82.5220° |
| perigee height: | 1174 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 46.2515° |
| argument of perigee: | 32.4234° |
| revolutions per day: | 12.79719280 |
| mean anomaly at epoch: | 329.0058° |
| orbit number at epoch: | 15093 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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