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 42844U 17042V 18267.70298216 +.00000134 +00000-0 +18582-4 0 9991
2 42844 097.5844 166.7742 0011391 213.8491 146.2002 14.91889985065195
| Epoch (UTC): | 24 September 2018 16:52:17 |
| Eccentricity: | 0.0011391 |
| inclination: | 97.5844° |
| perigee height: | 584 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 166.7742° |
| argument of perigee: | 213.8491° |
| revolutions per day: | 14.91889985 |
| mean anomaly at epoch: | 146.2002° |
| orbit number at epoch: | 6519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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