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 10674U 78018A 21023.86247356 -.00000039 00000-0 16670-4 0 9998
2 10674 69.3609 263.9476 0160318 86.0165 348.9568 13.43618552106250
| Epoch (UTC): | 23 January 2021 20:41:57 |
| Eccentricity: | 0.0160318 |
| inclination: | 69.3609° |
| perigee height: | 976 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 263.9476° |
| argument of perigee: | 86.0165° |
| revolutions per day: | 13.43618552 |
| mean anomaly at epoch: | 348.9568° |
| orbit number at epoch: | 10625 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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