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 22825U 26155.13386558 +.00000000 +00000-0 +72223-4 0 00000
2 22825 98.6882 222.5517 0009250 133.7828 226.4121 14.30938744 05
| Epoch (UTC): | 04 June 2026 03:12:45 |
| Eccentricity: | 0.0009250 |
| inclination: | 98.6882° |
| perigee height: | 782 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 222.5517° |
| argument of perigee: | 133.7828° |
| revolutions per day: | 14.30938744 |
| mean anomaly at epoch: | 226.4121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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