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 41868U 16061G 19320.65959124 +.00017856 +00000-0 +75993-4 0 9991
2 41868 042.7934 029.7502 0008574 042.3488 087.7355 15.84872588172029
| Epoch (UTC): | 16 November 2019 15:49:48 |
| Eccentricity: | 0.0008574 |
| inclination: | 42.7934° |
| perigee height: | 311 km |
| apogee height: | 322 km |
| right ascension of ascending node: | 29.7502° |
| argument of perigee: | 42.3488° |
| revolutions per day: | 15.84872588 |
| mean anomaly at epoch: | 87.7355° |
| orbit number at epoch: | 17202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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