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 13719U 82116B 17203.51828683 +.00000050 +00000-0 +19373-4 0 9995
2 13719 081.2563 325.7544 0070653 251.6266 157.2194 14.14607072785367
| Epoch (UTC): | 22 July 2017 12:26:19 |
| Eccentricity: | 0.0070653 |
| inclination: | 81.2563° |
| perigee height: | 792 km |
| apogee height: | 894 km |
| right ascension of ascending node: | 325.7544° |
| argument of perigee: | 251.6266° |
| revolutions per day: | 14.14607072 |
| mean anomaly at epoch: | 157.2194° |
| orbit number at epoch: | 78536 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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