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 18344.22183558 .00000088 00000-0 63381-4 0 9999
2 2680 39.4466 32.4828 0717454 278.3200 73.6863 13.37952883508260
| Epoch (UTC): | 10 December 2018 05:19:26 |
| Eccentricity: | 0.0717454 |
| inclination: | 39.4466° |
| perigee height: | 579 km |
| apogee height: | 1654 km |
| right ascension of ascending node: | 32.4828° |
| argument of perigee: | 278.3200° |
| revolutions per day: | 13.37952883 |
| mean anomaly at epoch: | 73.6863° |
| orbit number at epoch: | 50826 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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