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 50U 60009B 23333.72051204 -.00000068 00000-0 17230-3 0 9996
2 50 47.2278 169.7801 0113773 121.5455 239.6502 12.20135751824552
| Epoch (UTC): | 29 November 2023 17:17:32 |
| Eccentricity: | 0.0113773 |
| inclination: | 47.2278° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 169.7801° |
| argument of perigee: | 121.5455° |
| revolutions per day: | 12.20135751 |
| mean anomaly at epoch: | 239.6502° |
| orbit number at epoch: | 82455 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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