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 29U 60002B 19338.87605606 -.00000151 +00000-0 +85694-5 0 9996
2 29 048.3780 151.5895 0023751 116.2131 244.1226 14.74331341189684
| Epoch (UTC): | 04 December 2019 21:01:31 |
| Eccentricity: | 0.0023751 |
| inclination: | 48.3780° |
| perigee height: | 630 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 151.5895° |
| argument of perigee: | 116.2131° |
| revolutions per day: | 14.74331341 |
| mean anomaly at epoch: | 244.1226° |
| orbit number at epoch: | 18968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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