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 23336.66897602 -.00000036 00000-0 47390-3 0 9997
2 00050 47.2277 160.6280 0113780 130.3484 230.7306 12.20135902824451
| Epoch (UTC): | 02 December 2023 16:03:19 |
| Eccentricity: | 0.0113780 |
| inclination: | 47.2277° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 160.6280° |
| argument of perigee: | 130.3484° |
| revolutions per day: | 12.20135902 |
| mean anomaly at epoch: | 230.7306° |
| orbit number at epoch: | 82445 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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