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 18061.30351410 0.00000000 00000-0 00000-0 0 02
2 28384 63.1797 272.6328 7241004 272.5066 14.2295 2.00615000 03
| Epoch (UTC): | 02 March 2018 07:17:03 |
| Eccentricity: | 0.7241004 |
| inclination: | 63.1797° |
| perigee height: | 948 km |
| apogee height: | 39406 km |
| right ascension of ascending node: | 272.6328° |
| argument of perigee: | 272.5066° |
| revolutions per day: | 2.00615000 |
| mean anomaly at epoch: | 14.2295° |
| 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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