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 19316.73360251 -.00000048 +00000-0 +21921-4 0 9990
2 116 066.8118 020.4422 0074129 166.5461 193.7618 13.91761746961529
| Epoch (UTC): | 12 November 2019 17:36:23 |
| Eccentricity: | 0.0074129 |
| inclination: | 66.8118° |
| perigee height: | 868 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 20.4422° |
| argument of perigee: | 166.5461° |
| revolutions per day: | 13.91761746 |
| mean anomaly at epoch: | 193.7618° |
| orbit number at epoch: | 96152 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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