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 is defined by the following mean orbital elements,
1 45032U 13076V 20027.72226159 -.00000632 00000-0 -37238-2 0 9994
2 45032 82.4888 182.5390 0097326 38.3639 322.4319 12.58302260 2499
| Epoch (UTC): | 27 January 2020 17:20:03 |
| Eccentricity: | 0.0097326 |
| inclination: | 82.4888° |
| perigee height: | 1354 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 182.5390° |
| argument of perigee: | 38.3639° |
| revolutions per day: | 12.58302260 |
| mean anomaly at epoch: | 322.4319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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