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 27168U 02001A 19084.10400428 .00000086 00000-0 00000+0 0 9991
2 27168 8.3197 33.8363 0002074 336.7389 228.1033 1.00275908 5165
| Epoch (UTC): | 25 March 2019 02:29:45 |
| Eccentricity: | 0.0002074 |
| inclination: | 8.3197° |
| perigee height: | 35776 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 33.8363° |
| argument of perigee: | 336.7389° |
| revolutions per day: | 1.00275908 |
| mean anomaly at epoch: | 228.1033° |
| orbit number at epoch: | 516 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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