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 25260U 26088.21525795 +.00000000 +00000-0 +13049-3 0 00008
2 25260 98.2421 184.8664 0013731 108.7851 251.4838 14.56043403 06
| Epoch (UTC): | 29 March 2026 05:09:58 |
| Eccentricity: | 0.0013731 |
| inclination: | 98.2421° |
| perigee height: | 696 km |
| apogee height: | 716 km |
| right ascension of ascending node: | 184.8664° |
| argument of perigee: | 108.7851° |
| revolutions per day: | 14.56043403 |
| mean anomaly at epoch: | 251.4838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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