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 00050U 60009B 23331.50915999 -.00000055 00000-0 29508-3 0 9997
2 00050 47.2279 176.6440 0113765 114.9455 246.3203 12.20135703823825
| Epoch (UTC): | 27 November 2023 12:13:11 |
| Eccentricity: | 0.0113765 |
| inclination: | 47.2279° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 176.6440° |
| argument of perigee: | 114.9455° |
| revolutions per day: | 12.20135703 |
| mean anomaly at epoch: | 246.3203° |
| orbit number at epoch: | 82382 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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