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 21026.49515237 -.00000085 00000-0 -55427-5 0 9990
2 50 47.2311 149.0240 0113603 270.1589 88.6183 12.20114490697900
| Epoch (UTC): | 26 January 2021 11:53:01 |
| Eccentricity: | 0.0113603 |
| inclination: | 47.2311° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 149.0240° |
| argument of perigee: | 270.1589° |
| revolutions per day: | 12.20114490 |
| mean anomaly at epoch: | 88.6183° |
| orbit number at epoch: | 69790 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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