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 18174.90750537 +.00000032 +00000-0 +52285-4 0 9992
2 2680 039.4404 061.5228 0714225 038.0046 326.8941 13.37898724485112
| Epoch (UTC): | 23 June 2018 21:46:48 |
| Eccentricity: | 0.0714225 |
| inclination: | 39.4404° |
| perigee height: | 582 km |
| apogee height: | 1652 km |
| right ascension of ascending node: | 61.5228° |
| argument of perigee: | 38.0046° |
| revolutions per day: | 13.37898724 |
| mean anomaly at epoch: | 326.8941° |
| orbit number at epoch: | 48511 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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