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 32378U 07060A 19028.51656362 0.00000000 00000-0 00000-0 0 03
2 32378 62.8159 136.6490 7121929 266.2037 17.3198 2.00613000 03
| Epoch (UTC): | 28 January 2019 12:23:51 |
| Eccentricity: | 0.7121929 |
| inclination: | 62.8159° |
| perigee height: | 1265 km |
| apogee height: | 39090 km |
| right ascension of ascending node: | 136.6490° |
| argument of perigee: | 266.2037° |
| revolutions per day: | 2.00613000 |
| mean anomaly at epoch: | 17.3198° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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