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 19081.64735764 +.00000094 +00000-0 +72756-4 0 9999
2 2680 039.4398 299.2984 0717404 139.2724 226.3961 13.37989704521512
| Epoch (UTC): | 22 March 2019 15:32:11 |
| Eccentricity: | 0.0717404 |
| inclination: | 39.4398° |
| perigee height: | 579 km |
| apogee height: | 1654 km |
| right ascension of ascending node: | 299.2984° |
| argument of perigee: | 139.2724° |
| revolutions per day: | 13.37989704 |
| mean anomaly at epoch: | 226.3961° |
| orbit number at epoch: | 52151 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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