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 26088.07281020 +.00000000 +00000-0 +12173-3 0 00005
2 37227 71.9666 314.9847 0016859 264.8060 95.1182 14.85107858 02
| Epoch (UTC): | 29 March 2026 01:44:50 |
| Eccentricity: | 0.0016859 |
| inclination: | 71.9666° |
| perigee height: | 601 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 314.9847° |
| argument of perigee: | 264.8060° |
| revolutions per day: | 14.85107858 |
| mean anomaly at epoch: | 95.1182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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