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 25693U 99021A 18350.83206034 -.00000112 00000-0 47232-5 0 9997
2 25693 64.5555 237.6598 0042129 241.2394 118.4476 14.80823974 61251
| Epoch (UTC): | 16 December 2018 19:58:10 |
| Eccentricity: | 0.0042129 |
| inclination: | 64.5555° |
| perigee height: | 597 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 237.6598° |
| argument of perigee: | 241.2394° |
| revolutions per day: | 14.80823974 |
| mean anomaly at epoch: | 118.4476° |
| orbit number at epoch: | 6125 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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