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 19080.93847399 +.00000001 +00000-0 +20137-4 0 9995
2 29499 098.5864 136.5981 0002066 108.8303 017.8609 14.21544660644272
| Epoch (UTC): | 21 March 2019 22:31:24 |
| Eccentricity: | 0.0002066 |
| inclination: | 98.5864° |
| perigee height: | 818 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 136.5981° |
| argument of perigee: | 108.8303° |
| revolutions per day: | 14.21544660 |
| mean anomaly at epoch: | 17.8609° |
| orbit number at epoch: | 64427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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