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 37224U 26053.79234602 +.00000000 +00000-0 +29481-3 0 00007
2 37224 71.9732 339.3589 0016924 281.8432 78.0840 14.93185777 08
| Epoch (UTC): | 22 February 2026 19:00:58 |
| Eccentricity: | 0.0016924 |
| inclination: | 71.9732° |
| perigee height: | 576 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 339.3589° |
| argument of perigee: | 281.8432° |
| revolutions per day: | 14.93185777 |
| mean anomaly at epoch: | 78.0840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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