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 61925U 26145.17496681 +.00000000 +00000-0 +53171-3 0 00006
2 61925 42.9989 213.7569 0000899 285.7795 74.2957 15.27596554 01
| Epoch (UTC): | 25 May 2026 04:11:57 |
| Eccentricity: | 0.0000899 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 213.7569° |
| argument of perigee: | 285.7795° |
| revolutions per day: | 15.27596554 |
| mean anomaly at epoch: | 74.2957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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