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 23332.00057189 -.00000066 00000-0 19211-3 0 9993
2 00050 47.2279 175.1187 0113771 116.4119 244.8398 12.20135687823883
| Epoch (UTC): | 28 November 2023 00:00:49 |
| Eccentricity: | 0.0113771 |
| inclination: | 47.2279° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 175.1187° |
| argument of perigee: | 116.4119° |
| revolutions per day: | 12.20135687 |
| mean anomaly at epoch: | 244.8398° |
| orbit number at epoch: | 82388 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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