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 41848U 16067A 21334.19880693 .07289157 29045-5 20786-4 0 9993
2 41848 97.7650 148.0092 0015228 225.9629 247.4619 16.60370829279922
| Epoch (UTC): | 30 November 2021 04:46:16 |
| Eccentricity: | 0.0015228 |
| inclination: | 97.7650° |
| perigee height: | 102 km |
| apogee height: | 122 km |
| right ascension of ascending node: | 148.0092° |
| argument of perigee: | 225.9629° |
| revolutions per day: | 16.60370829 |
| mean anomaly at epoch: | 247.4619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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