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 27386U 02009A 21064.79405669 .00000034 00000-0 24781-4 0 9999
2 27386 98.1455 64.1648 0001293 92.9460 80.1220 14.38015104996176
| Epoch (UTC): | 05 March 2021 19:03:26 |
| Eccentricity: | 0.0001293 |
| inclination: | 98.1455° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 64.1648° |
| argument of perigee: | 92.9460° |
| revolutions per day: | 14.38015104 |
| mean anomaly at epoch: | 80.1220° |
| orbit number at epoch: | 99617 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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