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 26948U 01046A 20176.08831180 0.00000000 00000-0 00000-0 0 08
2 26948 10.8530 44.4700 0002091 202.0297 157.9381 1.00270000 05
| Epoch (UTC): | 24 June 2020 02:07:10 |
| Eccentricity: | 0.0002091 |
| inclination: | 10.8530° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 44.4700° |
| argument of perigee: | 202.0297° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 157.9381° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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