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 4256U 69082B 19083.51695710 -.00000038 00000-0 10459-4 0 9992
2 4256 70.0088 234.4328 0022057 279.8010 80.0606 13.98323396521107
| Epoch (UTC): | 24 March 2019 12:24:25 |
| Eccentricity: | 0.0022057 |
| inclination: | 70.0088° |
| perigee height: | 883 km |
| apogee height: | 915 km |
| right ascension of ascending node: | 234.4328° |
| argument of perigee: | 279.8010° |
| revolutions per day: | 13.98323396 |
| mean anomaly at epoch: | 80.0606° |
| orbit number at epoch: | 52110 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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