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 37673U 26039.04449306 +.00000000 +00000-0 +18419-3 0 00005
2 37673 97.9838 54.0652 0001592 111.6778 342.1992 14.78374877 08
| Epoch (UTC): | 08 February 2026 01:04:04 |
| Eccentricity: | 0.0001592 |
| inclination: | 97.9838° |
| perigee height: | 633 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 54.0652° |
| argument of perigee: | 111.6778° |
| revolutions per day: | 14.78374877 |
| mean anomaly at epoch: | 342.1992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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