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 00085U 61004C 22018.11072529 .00008121 00000-0 17168-2 0 9991
2 00085 38.7648 299.1369 0373866 49.3970 313.8684 14.23619325 13626
| Epoch (UTC): | 18 January 2022 02:39:26 |
| Eccentricity: | 0.0373866 |
| inclination: | 38.7648° |
| perigee height: | 544 km |
| apogee height: | 1082 km |
| right ascension of ascending node: | 299.1369° |
| argument of perigee: | 49.3970° |
| revolutions per day: | 14.23619325 |
| mean anomaly at epoch: | 313.8684° |
| orbit number at epoch: | 1362 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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