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 11425U 26088.18673074 +.00000000 +00000-0 +80769-4 0 00000
2 11425 74.0156 35.0387 0012906 121.6038 238.6376 14.34218869 04
| Epoch (UTC): | 29 March 2026 04:28:53 |
| Eccentricity: | 0.0012906 |
| inclination: | 74.0156° |
| perigee height: | 768 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 35.0387° |
| argument of perigee: | 121.6038° |
| revolutions per day: | 14.34218869 |
| mean anomaly at epoch: | 238.6376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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