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 37227U 26039.10078078 +.00000000 +00000-0 +16271-3 0 00005
2 37227 71.9653 64.4327 0015222 348.6174 11.4645 14.84972785 01
| Epoch (UTC): | 08 February 2026 02:25:07 |
| Eccentricity: | 0.0015222 |
| inclination: | 71.9653° |
| perigee height: | 603 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 64.4327° |
| argument of perigee: | 348.6174° |
| revolutions per day: | 14.84972785 |
| mean anomaly at epoch: | 11.4645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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