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 41466U 16026C 22062.43880789 .07985188 24080-5 16740-2 0 9990
2 41466 97.1087 340.3702 0002849 146.1677 213.9800 16.31028938329401
| Epoch (UTC): | 03 March 2022 10:31:53 |
| Eccentricity: | 0.0002849 |
| inclination: | 97.1087° |
| perigee height: | 188 km |
| apogee height: | 191 km |
| right ascension of ascending node: | 340.3702° |
| argument of perigee: | 146.1677° |
| revolutions per day: | 16.31028938 |
| mean anomaly at epoch: | 213.9800° |
| orbit number at epoch: | 32940 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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