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 26549U 00057E 18145.45101829 -.00000006 00000-0 16908-4 0 9992
2 26549 64.5495 141.8712 0006513 114.8119 245.3665 14.83474214954417
| Epoch (UTC): | 25 May 2018 10:49:27 |
| Eccentricity: | 0.0006513 |
| inclination: | 64.5495° |
| perigee height: | 614 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 141.8712° |
| argument of perigee: | 114.8119° |
| revolutions per day: | 14.83474214 |
| mean anomaly at epoch: | 245.3665° |
| orbit number at epoch: | 95441 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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