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 21026.16916161 -.00000071 00000-0 48285-5 0 9994
2 116 66.8107 23.7494 0079451 217.0231 142.5351 13.91781982 23295
| Epoch (UTC): | 26 January 2021 04:03:35 |
| Eccentricity: | 0.0079451 |
| inclination: | 66.8107° |
| perigee height: | 864 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 23.7494° |
| argument of perigee: | 217.0231° |
| revolutions per day: | 13.91781982 |
| mean anomaly at epoch: | 142.5351° |
| orbit number at epoch: | 2329 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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