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 39434U 13066U 18175.14990873 .00002303 00000-0 16995-3 0 9993
2 39434 97.6180 250.7659 0032579 343.2309 16.7864 15.03862539250708
| Epoch (UTC): | 24 June 2018 03:35:52 |
| Eccentricity: | 0.0032579 |
| inclination: | 97.6180° |
| perigee height: | 532 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 250.7659° |
| argument of perigee: | 343.2309° |
| revolutions per day: | 15.03862539 |
| mean anomaly at epoch: | 16.7864° |
| orbit number at epoch: | 25070 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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