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 41607U 16040J 21023.72870038 .00001838 00000-0 76072-4 0 9998
2 41607 97.2899 83.6340 0014224 125.9717 234.2843 15.25104344254986
| Epoch (UTC): | 23 January 2021 17:29:19 |
| Eccentricity: | 0.0014224 |
| inclination: | 97.2899° |
| perigee height: | 481 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 83.6340° |
| argument of perigee: | 125.9717° |
| revolutions per day: | 15.25104344 |
| mean anomaly at epoch: | 234.2843° |
| orbit number at epoch: | 25498 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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