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 21023.15101947 -.00000078 00000-0 -41998-6 0 9991
2 116 66.8104 31.1281 0079670 219.0172 140.5144 13.91781895 22872
| Epoch (UTC): | 23 January 2021 03:37:28 |
| Eccentricity: | 0.0079670 |
| inclination: | 66.8104° |
| perigee height: | 864 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 31.1281° |
| argument of perigee: | 219.0172° |
| revolutions per day: | 13.91781895 |
| mean anomaly at epoch: | 140.5144° |
| orbit number at epoch: | 2287 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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