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 08344U 75094B 22148.92193491 .00000177 00000-0 65475-4 0 9995
2 08344 74.0587 36.0831 0022400 206.7482 153.2520 14.39259128445308
| Epoch (UTC): | 28 May 2022 22:07:35 |
| Eccentricity: | 0.0022400 |
| inclination: | 74.0587° |
| perigee height: | 745 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 36.0831° |
| argument of perigee: | 206.7482° |
| revolutions per day: | 14.39259128 |
| mean anomaly at epoch: | 153.2520° |
| orbit number at epoch: | 44530 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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