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 27844U 03031E 19340.61227439 .00000051 00000-0 42506-4 0 9990
2 27844 98.6839 346.2696 0008851 255.1191 104.9007 14.22209261852580
| Epoch (UTC): | 06 December 2019 14:41:40 |
| Eccentricity: | 0.0008851 |
| inclination: | 98.6839° |
| perigee height: | 811 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 346.2696° |
| argument of perigee: | 255.1191° |
| revolutions per day: | 14.22209261 |
| mean anomaly at epoch: | 104.9007° |
| orbit number at epoch: | 85258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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