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 39437U 13066X 19043.80300038 .12796154 26637-5 18530-2 0 9994
2 39437 97.7085 195.7342 0011516 316.0404 43.9974 16.34536523289943
| Epoch (UTC): | 12 February 2019 19:16:19 |
| Eccentricity: | 0.0011516 |
| inclination: | 97.7085° |
| perigee height: | 173 km |
| apogee height: | 188 km |
| right ascension of ascending node: | 195.7342° |
| argument of perigee: | 316.0404° |
| revolutions per day: | 16.34536523 |
| mean anomaly at epoch: | 43.9974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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