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 21017.18659610 -.00000083 00000-0 -45435-5 0 9997
2 116 66.8085 45.7101 0080048 222.9366 136.5447 13.91781802 22049
| Epoch (UTC): | 17 January 2021 04:28:41 |
| Eccentricity: | 0.0080048 |
| inclination: | 66.8085° |
| perigee height: | 864 km |
| apogee height: | 981 km |
| right ascension of ascending node: | 45.7101° |
| argument of perigee: | 222.9366° |
| revolutions per day: | 13.91781802 |
| mean anomaly at epoch: | 136.5447° |
| orbit number at epoch: | 2204 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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