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 28384U 04034A 18220.80467123 0.00000000 00000-0 00000-0 0 03
2 28384 63.1745 250.5073 7162039 272.6696 14.7417 2.00615000 09
| Epoch (UTC): | 08 August 2018 19:18:43 |
| Eccentricity: | 0.7162039 |
| inclination: | 63.1745° |
| perigee height: | 1158 km |
| apogee height: | 39196 km |
| right ascension of ascending node: | 250.5073° |
| argument of perigee: | 272.6696° |
| revolutions per day: | 2.00615000 |
| mean anomaly at epoch: | 14.7417° |
| 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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