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 22227.81194368 .00000480 00000-0 81550-4 0 9994
2 37673 98.0039 235.6225 0000798 68.9431 104.1543 14.73514142601059
| Epoch (UTC): | 15 August 2022 19:29:11 |
| Eccentricity: | 0.0000798 |
| inclination: | 98.0039° |
| perigee height: | 649 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 235.6225° |
| argument of perigee: | 68.9431° |
| revolutions per day: | 14.73514142 |
| mean anomaly at epoch: | 104.1543° |
| orbit number at epoch: | 60105 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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