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 00226U 26152.22013354 +.00000000 +00000-0 +52414-4 0 00009
2 00226 48.2959 83.0451 0076000 186.8980 173.0879 14.47180226 03
| Epoch (UTC): | 01 June 2026 05:16:59 |
| Eccentricity: | 0.0076000 |
| inclination: | 48.2959° |
| perigee height: | 681 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 83.0451° |
| argument of perigee: | 186.8980° |
| revolutions per day: | 14.47180226 |
| mean anomaly at epoch: | 173.0879° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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