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 37728U 11029A 18062.68209158 0.00200000 00000-0 29320-3 0 00
2 37728 39.9189 230.3239 0004163 47.7711 312.2281 16.04002245 04
| Epoch (UTC): | 03 March 2018 16:22:12 |
| Eccentricity: | 0.0004163 |
| inclination: | 39.9189° |
| perigee height: | 260 km |
| apogee height: | 266 km |
| right ascension of ascending node: | 230.3239° |
| argument of perigee: | 47.7711° |
| revolutions per day: | 16.04002245 |
| mean anomaly at epoch: | 312.2281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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