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 is defined by the following mean orbital elements,
1 42949U 17066A 21249.71417234 0.00000000 00000-0 00000-0 0 08
2 42949 2.8159 335.1754 0003938 138.6479 221.3984 1.00270000 03
| Epoch (UTC): | 06 September 2021 17:08:24 |
| Eccentricity: | 0.0003938 |
| inclination: | 2.8159° |
| perigee height: | 35770 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 335.1754° |
| argument of perigee: | 138.6479° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 221.3984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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