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 39250U 13048B 18260.47933051 +.00000041 +00000-0 +22530-3 0 9994
2 39250 082.4850 307.8776 0016963 298.1596 061.7764 12.42928057227520
| Epoch (UTC): | 17 September 2018 11:30:14 |
| Eccentricity: | 0.0016963 |
| inclination: | 82.4850° |
| perigee height: | 1481 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 307.8776° |
| argument of perigee: | 298.1596° |
| revolutions per day: | 12.42928057 |
| mean anomaly at epoch: | 61.7764° |
| orbit number at epoch: | 22752 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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