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 37673U 11024A 23151.93207240 .00001155 00000-0 18171-3 0 9996
2 37673 97.9998 160.9731 0002284 90.3503 331.6529 14.74394091643646
| Epoch (UTC): | 31 May 2023 22:22:11 |
| Eccentricity: | 0.0002284 |
| inclination: | 97.9998° |
| perigee height: | 645 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 160.9731° |
| argument of perigee: | 90.3503° |
| revolutions per day: | 14.74394091 |
| mean anomaly at epoch: | 331.6529° |
| orbit number at epoch: | 64364 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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