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 25994U 99068A 18116.20120344 .00000020 00000-0 14574-4 0 9991
2 25994 98.2051 191.8160 0000883 87.5930 272.5415 14.57096549976258
| Epoch (UTC): | 26 April 2018 04:49:43 |
| Eccentricity: | 0.0000883 |
| inclination: | 98.2051° |
| perigee height: | 702 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 191.8160° |
| argument of perigee: | 87.5930° |
| revolutions per day: | 14.57096549 |
| mean anomaly at epoch: | 272.5415° |
| orbit number at epoch: | 97625 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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