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 29049U 06011C 19054.19216955 .00000035 00000-0 29934-4 0 9998
2 29049 72.0193 90.5577 0034363 161.8515 198.3857 14.28698243671009
| Epoch (UTC): | 23 February 2019 04:36:43 |
| Eccentricity: | 0.0034363 |
| inclination: | 72.0193° |
| perigee height: | 771 km |
| apogee height: | 821 km |
| right ascension of ascending node: | 90.5577° |
| argument of perigee: | 161.8515° |
| revolutions per day: | 14.28698243 |
| mean anomaly at epoch: | 198.3857° |
| orbit number at epoch: | 67100 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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