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 25399U 26106.72190244 +.00000000 +00000-0 +37376-4 0 00005
2 25399 98.9744 92.3387 0000908 318.1911 41.9198 14.25604073 08
| Epoch (UTC): | 16 April 2026 17:19:32 |
| Eccentricity: | 0.0000908 |
| inclination: | 98.9744° |
| perigee height: | 806 km |
| apogee height: | 807 km |
| right ascension of ascending node: | 92.3387° |
| argument of perigee: | 318.1911° |
| revolutions per day: | 14.25604073 |
| mean anomaly at epoch: | 41.9198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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