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 26960U 01049D 20024.51680606 .00000616 00000-0 43027-4 0 9990
2 26960 97.8006 15.4222 0054842 172.0103 188.2011 15.08092347997395
| Epoch (UTC): | 24 January 2020 12:24:12 |
| Eccentricity: | 0.0054842 |
| inclination: | 97.8006° |
| perigee height: | 504 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 15.4222° |
| argument of perigee: | 172.0103° |
| revolutions per day: | 15.08092347 |
| mean anomaly at epoch: | 188.2011° |
| orbit number at epoch: | 99739 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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