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 37225U 26032.49348123 +.00000000 +00000-0 +88071-4 0 00007
2 37225 71.9718 101.4759 0016037 15.6070 344.5585 14.81957706 09
| Epoch (UTC): | 01 February 2026 11:50:36 |
| Eccentricity: | 0.0016037 |
| inclination: | 71.9718° |
| perigee height: | 612 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 101.4759° |
| argument of perigee: | 15.6070° |
| revolutions per day: | 14.81957706 |
| mean anomaly at epoch: | 344.5585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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