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 27424U 02022A 19290.90759132 +.00000103 +00000-0 +32886-4 0 9997
2 27424 098.2049 229.9576 0002704 046.2357 026.6148 14.57113745928401
| Epoch (UTC): | 17 October 2019 21:46:55 |
| Eccentricity: | 0.0002704 |
| inclination: | 98.2049° |
| perigee height: | 700 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 229.9576° |
| argument of perigee: | 46.2357° |
| revolutions per day: | 14.57113745 |
| mean anomaly at epoch: | 26.6148° |
| orbit number at epoch: | 92840 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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