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 2680U 67014A 18267.55327096 +.00000155 +00000-0 +91957-4 0 9991
2 2680 039.4437 011.6711 0715687 203.5879 153.0432 13.37924310497521
| Epoch (UTC): | 24 September 2018 13:16:42 |
| Eccentricity: | 0.0715687 |
| inclination: | 39.4437° |
| perigee height: | 580 km |
| apogee height: | 1653 km |
| right ascension of ascending node: | 11.6711° |
| argument of perigee: | 203.5879° |
| revolutions per day: | 13.37924310 |
| mean anomaly at epoch: | 153.0432° |
| orbit number at epoch: | 49752 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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