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 19145.51844707 -.00000138 00000-0 10485-4 0 9990
2 29 48.3806 344.0464 0024011 7.5999 352.5272 14.74304768161271
| Epoch (UTC): | 25 May 2019 12:26:33 |
| Eccentricity: | 0.0024011 |
| inclination: | 48.3806° |
| perigee height: | 630 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 344.0464° |
| argument of perigee: | 7.5999° |
| revolutions per day: | 14.74304768 |
| mean anomaly at epoch: | 352.5272° |
| orbit number at epoch: | 16127 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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