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 is defined by the following mean orbital elements,
1 44049U 19009B 19079.85416667 -.00057171 +00000-0 +00000-0 0 9991
2 44049 025.0088 010.5463 9637541 181.7585 043.0154 00.08972053000129
| Epoch (UTC): | 20 March 2019 20:30:00 |
| Eccentricity: | 0.9637541 |
| inclination: | 25.0088° |
| perigee height: | 1261 km |
| apogee height: | 407516 km |
| right ascension of ascending node: | 10.5463° |
| argument of perigee: | 181.7585° |
| revolutions per day: | 0.08972053 |
| mean anomaly at epoch: | 43.0154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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