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 37227U 10062F 23274.48664095 .00001924 00000-0 25379-3 0 9995
2 37227 71.9697 182.1539 0015694 182.7036 177.4046 14.81201196219108
| Epoch (UTC): | 01 October 2023 11:40:45 |
| Eccentricity: | 0.0015694 |
| inclination: | 71.9697° |
| perigee height: | 614 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 182.1539° |
| argument of perigee: | 182.7036° |
| revolutions per day: | 14.81201196 |
| mean anomaly at epoch: | 177.4046° |
| orbit number at epoch: | 21910 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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