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 27945U 03042G 19340.64613470 -.00000007 00000-0 76445-5 0 9993
2 27945 98.0690 108.2747 0010828 277.5091 82.4882 14.64856623865163
| Epoch (UTC): | 06 December 2019 15:30:26 |
| Eccentricity: | 0.0010828 |
| inclination: | 98.0690° |
| perigee height: | 670 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 108.2747° |
| argument of perigee: | 277.5091° |
| revolutions per day: | 14.64856623 |
| mean anomaly at epoch: | 82.4882° |
| orbit number at epoch: | 86516 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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