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 42932U 17052A 19106.10363451 0.00000000 00000-0 00000-0 0 08
2 42932 54.5148 156.4405 0011000 131.5229 228.4770 15.84488599 00
| Epoch (UTC): | 16 April 2019 02:29:14 |
| Eccentricity: | 0.0011000 |
| inclination: | 54.5148° |
| perigee height: | 310 km |
| apogee height: | 325 km |
| right ascension of ascending node: | 156.4405° |
| argument of perigee: | 131.5229° |
| revolutions per day: | 15.84488599 |
| mean anomaly at epoch: | 228.4770° |
| 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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