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 26138.46020873 +.00000000 +00000-0 +11803-3 0 00007
2 37224 71.9681 147.6682 0012773 128.2058 232.0265 14.93605517 03
| Epoch (UTC): | 18 May 2026 11:02:42 |
| Eccentricity: | 0.0012773 |
| inclination: | 71.9681° |
| perigee height: | 578 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 147.6682° |
| argument of perigee: | 128.2058° |
| revolutions per day: | 14.93605517 |
| mean anomaly at epoch: | 232.0265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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