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 20275.46758592 -.00000051 +00000-0 +19966-4 0 9995
2 116 066.8096 309.0532 0081956 292.3622 066.8787 13.91775792006584
| Epoch (UTC): | 01 October 2020 11:13:19 |
| Eccentricity: | 0.0081956 |
| inclination: | 66.8096° |
| perigee height: | 862 km |
| apogee height: | 982 km |
| right ascension of ascending node: | 309.0532° |
| argument of perigee: | 292.3622° |
| revolutions per day: | 13.91775792 |
| mean anomaly at epoch: | 66.8787° |
| orbit number at epoch: | 658 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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