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 26088.14549461 +.00000000 +00000-0 +83409-4 0 00009
2 00226 48.2979 13.0968 0076609 282.4512 76.7823 14.47156459 09
| Epoch (UTC): | 29 March 2026 03:29:30 |
| Eccentricity: | 0.0076609 |
| inclination: | 48.2979° |
| perigee height: | 680 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 13.0968° |
| argument of perigee: | 282.4512° |
| revolutions per day: | 14.47156459 |
| mean anomaly at epoch: | 76.7823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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