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 26053.67307361 +.00000000 +00000-0 +54421-4 0 00001
2 22825 98.7017 121.0695 0009452 78.8586 281.3658 14.30907583 02
| Epoch (UTC): | 22 February 2026 16:09:13 |
| Eccentricity: | 0.0009452 |
| inclination: | 98.7017° |
| perigee height: | 782 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 121.0695° |
| argument of perigee: | 78.8586° |
| revolutions per day: | 14.30907583 |
| mean anomaly at epoch: | 281.3658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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