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 42849U 17042AA 21016.15418377 .00000243 00000-0 28775-4 0 9999
2 42849 97.4962 256.6066 0006671 291.5509 68.5000 14.92613727191134
| Epoch (UTC): | 16 January 2021 03:42:01 |
| Eccentricity: | 0.0006671 |
| inclination: | 97.4962° |
| perigee height: | 585 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 256.6066° |
| argument of perigee: | 291.5509° |
| revolutions per day: | 14.92613727 |
| mean anomaly at epoch: | 68.5000° |
| orbit number at epoch: | 19113 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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