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 18295.57116306 0.00000000 00000-0 00000-0 0 03
2 28384 63.3301 240.5359 7152309 272.6950 14.8076 2.00620000 05
| Epoch (UTC): | 22 October 2018 13:42:28 |
| Eccentricity: | 0.7152309 |
| inclination: | 63.3301° |
| perigee height: | 1184 km |
| apogee height: | 39170 km |
| right ascension of ascending node: | 240.5359° |
| argument of perigee: | 272.6950° |
| revolutions per day: | 2.00620000 |
| mean anomaly at epoch: | 14.8076° |
| 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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