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 22826U 26066.12951425 +.00000000 +00000-0 +73924-4 0 00001
2 22826 98.6935 133.4450 0009335 30.2249 329.9471 14.31335939 08
| Epoch (UTC): | 07 March 2026 03:06:30 |
| Eccentricity: | 0.0009335 |
| inclination: | 98.6935° |
| perigee height: | 781 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 133.4450° |
| argument of perigee: | 30.2249° |
| revolutions per day: | 14.31335939 |
| mean anomaly at epoch: | 329.9471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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