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 37223U 26140.33612515 +.00000000 +00000-0 +18066-3 0 00003
2 37223 71.9686 103.2980 0011325 89.2983 270.9488 15.00137823 08
| Epoch (UTC): | 20 May 2026 08:04:01 |
| Eccentricity: | 0.0011325 |
| inclination: | 71.9686° |
| perigee height: | 559 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 103.2980° |
| argument of perigee: | 89.2983° |
| revolutions per day: | 15.00137823 |
| mean anomaly at epoch: | 270.9488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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