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 28158U 04004A 19049.93261010 -.00000230 +00000-0 +00000-0 0 9993
2 28158 008.5477 042.0045 0000832 356.2277 173.4375 01.00269374006106
| Epoch (UTC): | 18 February 2019 22:22:57 |
| Eccentricity: | 0.0000832 |
| inclination: | 8.5477° |
| perigee height: | 35783 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 42.0045° |
| argument of perigee: | 356.2277° |
| revolutions per day: | 1.00269374 |
| mean anomaly at epoch: | 173.4375° |
| orbit number at epoch: | 610 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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