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 26128.21280846 +.00000000 +00000-0 +15006-3 0 00006
2 37224 71.9690 170.8750 0013359 149.7054 210.4892 14.93580287 04
| Epoch (UTC): | 08 May 2026 05:06:26 |
| Eccentricity: | 0.0013359 |
| inclination: | 71.9690° |
| perigee height: | 577 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 170.8750° |
| argument of perigee: | 149.7054° |
| revolutions per day: | 14.93580287 |
| mean anomaly at epoch: | 210.4892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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