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 28359U 04022B 22137.74749983 .00008333 00000-0 82380-3 0 9992
2 28359 49.5433 38.0779 4633126 329.5868 10.2483 6.27827529397237
| Epoch (UTC): | 17 May 2022 17:56:23 |
| Eccentricity: | 0.4633126 |
| inclination: | 49.5433° |
| perigee height: | 283 km |
| apogee height: | 11784 km |
| right ascension of ascending node: | 38.0779° |
| argument of perigee: | 329.5868° |
| revolutions per day: | 6.27827529 |
| mean anomaly at epoch: | 10.2483° |
| orbit number at epoch: | 39723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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