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 19258.23819465 -.00000027 00000-0 38022-4 0 9993
2 116 66.8100 163.4391 0078947 207.0269 152.6690 13.91758691953869
| Epoch (UTC): | 15 September 2019 05:43:00 |
| Eccentricity: | 0.0078947 |
| inclination: | 66.8100° |
| perigee height: | 865 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 163.4391° |
| argument of perigee: | 207.0269° |
| revolutions per day: | 13.91758691 |
| mean anomaly at epoch: | 152.6690° |
| orbit number at epoch: | 95386 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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