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 41874U 16062F 19345.58720658 +.00000555 +00000-0 +35023-4 0 9994
2 41874 051.6537 086.3784 0012095 179.0151 181.0854 15.25598687169302
| Epoch (UTC): | 11 December 2019 14:05:34 |
| Eccentricity: | 0.0012095 |
| inclination: | 51.6537° |
| perigee height: | 480 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 86.3784° |
| argument of perigee: | 179.0151° |
| revolutions per day: | 15.25598687 |
| mean anomaly at epoch: | 181.0854° |
| orbit number at epoch: | 16930 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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