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 47930U 98067SG 22104.40989677 .03524807 11894-4 16214-2 0 9994
2 47930 51.6157 260.0446 0013462 303.1008 56.8718 16.20863404 61841
| Epoch (UTC): | 14 April 2022 09:50:15 |
| Eccentricity: | 0.0013462 |
| inclination: | 51.6157° |
| perigee height: | 208 km |
| apogee height: | 226 km |
| right ascension of ascending node: | 260.0446° |
| argument of perigee: | 303.1008° |
| revolutions per day: | 16.20863404 |
| mean anomaly at epoch: | 56.8718° |
| orbit number at epoch: | 6184 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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