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 37170U 10049A 22288.52086201 .04431479 53169-5 33323-4 0 9997
2 37170 63.6108 331.4830 0917237 243.9434 288.7012 14.48103420 90345
| Epoch (UTC): | 15 October 2022 12:30:02 |
| Eccentricity: | 0.0917237 |
| inclination: | 63.6108° |
| perigee height: | 80 km |
| apogee height: | 1384 km |
| right ascension of ascending node: | 331.4830° |
| argument of perigee: | 243.9434° |
| revolutions per day: | 14.48103420 |
| mean anomaly at epoch: | 288.7012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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