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 42732U 98067MM 19035.84948260 .08466551 12392-4 69401-3 0 9996
2 42732 51.6102 222.7661 0006965 282.1368 217.9093 16.38912453 97286
| Epoch (UTC): | 04 February 2019 20:23:15 |
| Eccentricity: | 0.0006965 |
| inclination: | 51.6102° |
| perigee height: | 164 km |
| apogee height: | 173 km |
| right ascension of ascending node: | 222.7661° |
| argument of perigee: | 282.1368° |
| revolutions per day: | 16.38912453 |
| mean anomaly at epoch: | 217.9093° |
| orbit number at epoch: | 9728 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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