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 29050U 06011D 19054.07501038 .00000083 00000-0 27805-4 0 9994
2 29050 72.0150 285.9268 0048394 119.0882 241.5129 14.58765436686373
| Epoch (UTC): | 23 February 2019 01:48:00 |
| Eccentricity: | 0.0048394 |
| inclination: | 72.0150° |
| perigee height: | 663 km |
| apogee height: | 731 km |
| right ascension of ascending node: | 285.9268° |
| argument of perigee: | 119.0882° |
| revolutions per day: | 14.58765436 |
| mean anomaly at epoch: | 241.5129° |
| orbit number at epoch: | 68637 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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