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 37380U 10062M 22272.46651314 .00000656 00000-0 94553-4 0 9992
2 37380 71.9702 283.1759 0015342 146.8995 213.3131 14.79766705164750
| Epoch (UTC): | 29 September 2022 11:11:46 |
| Eccentricity: | 0.0015342 |
| inclination: | 71.9702° |
| perigee height: | 619 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 283.1759° |
| argument of perigee: | 146.8995° |
| revolutions per day: | 14.79766705 |
| mean anomaly at epoch: | 213.3131° |
| orbit number at epoch: | 16475 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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