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 116U 61015A 19200.82061710 -.00000022 00000-0 42345-4 0 9995
2 116 66.8109 303.8025 0082171 244.8845 114.3693 13.91755699945870
| Epoch (UTC): | 19 July 2019 19:41:41 |
| Eccentricity: | 0.0082171 |
| inclination: | 66.8109° |
| perigee height: | 862 km |
| apogee height: | 982 km |
| right ascension of ascending node: | 303.8025° |
| argument of perigee: | 244.8845° |
| revolutions per day: | 13.91755699 |
| mean anomaly at epoch: | 114.3693° |
| orbit number at epoch: | 94587 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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