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 22237U 92080B 23150.40713899 .00000362 00000-0 46054-4 0 9991
2 22237 82.5125 255.7288 0018133 299.9608 59.9804 14.78863279644450
| Epoch (UTC): | 30 May 2023 09:46:16 |
| Eccentricity: | 0.0018133 |
| inclination: | 82.5125° |
| perigee height: | 620 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 255.7288° |
| argument of perigee: | 299.9608° |
| revolutions per day: | 14.78863279 |
| mean anomaly at epoch: | 59.9804° |
| orbit number at epoch: | 64445 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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