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 29048U 06011B 18322.53370685 .00000074 00000-0 45473-4 0 9992
2 29048 71.9653 118.9943 0045602 292.6310 67.0007 14.28601441661410
| Epoch (UTC): | 18 November 2018 12:48:32 |
| Eccentricity: | 0.0045602 |
| inclination: | 71.9653° |
| perigee height: | 763 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 118.9943° |
| argument of perigee: | 292.6310° |
| revolutions per day: | 14.28601441 |
| mean anomaly at epoch: | 67.0007° |
| orbit number at epoch: | 66141 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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