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 29499U 06044A 18263.77553299 -.00000017 +00000-0 +11844-4 0 9995
2 29499 098.6173 319.0608 0000319 058.8473 050.3768 14.21529345618396
| Epoch (UTC): | 20 September 2018 18:36:46 |
| Eccentricity: | 0.0000319 |
| inclination: | 98.6173° |
| perigee height: | 820 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 319.0608° |
| argument of perigee: | 58.8473° |
| revolutions per day: | 14.21529345 |
| mean anomaly at epoch: | 50.3768° |
| orbit number at epoch: | 61839 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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