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 10974U 78067B 23151.82430220 .00000536 00000-0 55637-4 0 9996
2 10974 82.4819 269.0847 0016482 340.1751 19.8824 14.87984818409680
| Epoch (UTC): | 31 May 2023 19:46:59 |
| Eccentricity: | 0.0016482 |
| inclination: | 82.4819° |
| perigee height: | 593 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 269.0847° |
| argument of perigee: | 340.1751° |
| revolutions per day: | 14.87984818 |
| mean anomaly at epoch: | 19.8824° |
| orbit number at epoch: | 40968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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