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 25161U 26088.24000786 +.00000000 +00000-0 +23098-3 0 00004
2 25161 107.9914 270.7458 0058600 192.6151 262.6842 14.28227863 08
| Epoch (UTC): | 29 March 2026 05:45:36 |
| Eccentricity: | 0.0058600 |
| inclination: | 107.9914° |
| perigee height: | 756 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 270.7458° |
| argument of perigee: | 192.6151° |
| revolutions per day: | 14.28227863 |
| mean anomaly at epoch: | 262.6842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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