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 42789U 17036AA 19077.64801061 +.00001402 +00000-0 +63338-4 0 9991
2 42789 097.3634 137.6300 0011443 184.9838 175.1286 15.22555376096262
| Epoch (UTC): | 18 March 2019 15:33:08 |
| Eccentricity: | 0.0011443 |
| inclination: | 97.3634° |
| perigee height: | 490 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 137.6300° |
| argument of perigee: | 184.9838° |
| revolutions per day: | 15.22555376 |
| mean anomaly at epoch: | 175.1286° |
| orbit number at epoch: | 9626 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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