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 42705U 98067LN 18276.06534946 +.17607533 +12691-4 +36390-3 0 9998
2 42705 051.6425 140.2579 0007226 336.1768 024.0803 16.46477481079261
| Epoch (UTC): | 03 October 2018 01:34:06 |
| Eccentricity: | 0.0007226 |
| inclination: | 51.6425° |
| perigee height: | 144 km |
| apogee height: | 153 km |
| right ascension of ascending node: | 140.2579° |
| argument of perigee: | 336.1768° |
| revolutions per day: | 16.46477481 |
| mean anomaly at epoch: | 24.0803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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