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 27422U 02021B 17289.55131302 -.00000012 +00000-0 +11209-4 0 9990
2 27422 098.2372 283.1601 0011237 233.8831 126.1312 14.29257485805908
| Epoch (UTC): | 16 October 2017 13:13:53 |
| Eccentricity: | 0.0011237 |
| inclination: | 98.2372° |
| perigee height: | 786 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 283.1601° |
| argument of perigee: | 233.8831° |
| revolutions per day: | 14.29257485 |
| mean anomaly at epoch: | 126.1312° |
| orbit number at epoch: | 80590 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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